Author's personal copy Chemie der Erde 70 (2010) 199–219 Contents lists available at ScienceDirect Chemie der Erde journal homepage: www.elsevier.de/chemer INVITED REVIEW Similar-sized collisions and the diversity of planets Erik Asphaug Earth and Planetary Sciences, University of California, 1156 High Street, Santa Cruz, CA 95064, USA a r t i c l e in fo abstract Article history: Received 10 September 2009 Accepted 31 January 2010 It is assumed in models of terrestrial planet formation that colliding bodies simply merge. From this the dynamical and chemical properties (and habitability) of finished planets have been computed, and our own and other planetary systems compared to the results of these calculations. But efficient mergers may be exceptions to the rule, for the similar-sized collisions (SSCs) that dominate terrestrial planet formation, simply because moderately off-axis SSCs are grazing; their centers of mass overshoot. In a ‘‘hit and run’’ collision the smaller body narrowly avoids accretion and is profoundly deformed and altered by gravitational and mechanical torques, shears, tides, and impact shocks. Consequences to the larger body are minor in inverse proportion to its relative mass. Over the possible impact angles, hitand-run is the most common outcome for impact velocities vimp between 1:2 and 2.7 times the mutual escape velocity vesc between similar-sized planets. Slower collisions are usually accretionary, and faster SSCs are erosive or disruptive, and thus the prevalence of hit-and-run is sensitive to the velocity regime during epochs of accretion. Consequences of hit-and-run are diverse. If barely grazing, the target strips much of the exterior from the impactor—any atmosphere and ocean, much of the crust—and unloads its deep interior from hydrostatic pressure for about an hour. If closer to head-on ð 302451Þ a hit-and-run can cause the impactor core to plow through the target mantle, graze the target core, and emerge as a chain of diverse new planetoids on escaping trajectories. A hypothesis is developed for the diversity of next-largest bodies (NLBs) in an accreting planetary system—the bodies from which asteroids and meteorites derive. Because nearly all the NLBs eventually get accreted by the largest (Venus and Earth in our terrestrial system) or by the Sun, or otherwise lost, those we see today have survived the attrition of merger, evolving with each close call towards denser and volatile-poor bulk composition. This hypothesis would explain the observed density diversity of differentiated asteroids, and of dwarf planets beyond Neptune, in terms of episodic global-scale losses of rock or ice mantles, respectively. In an event similar to the Moon-forming giant impact, Mercury might have lost its original crust and upper mantle when it emerged from a modest velocity hit and run collision with a larger embryo or planet. In systems with super-Earths, profound diversity and diminished habitability is predicted among the unaccreted Earth-mass planets, as many of these will have be stripped of their atmospheres, oceans and crusts. & 2010 Elsevier GmbH. All rights reserved. Keywords: Planets Impact Collisions Accretion Planet Formation 1. Introduction impact velocities vimp comparable to the mutual escape velocity During the late stage of terrestrial planet formation (Wetherill, 1985), giant impacts occur when similar-sized planets at or near the largest end of their size distribution collide at speeds ranging from 1 to a few times their mutual escape velocity vesc. This notion of late giant impacts emerged alongside the idea for a giant impact origin of the Moon (Hartmann and Davis, 1975), where a Mars-sized projectile is proposed to have struck the proto-Earth to liberate a new planet composed mostly of Earth-like mantle. Giant impacts can be generalized as occurring between the largest and next-largest bodies at any stage of planet formation, at vesc ¼ Tel.: + 1 831 459 2260; fax: +1 831 459 3074. E-mail address: [email protected] 0009-2819/$ - see front matter & 2010 Elsevier GmbH. All rights reserved. doi:10.1016/j.chemer.2010.01.004 rffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi Mþm 2G Rþr ð1Þ which is the velocity at which two spheres collide if starting out at zero velocity at infinite distance. The radii r t R and masses m and M correspond to a spherical projectile and target, and G ¼ 6:673 108 cm2 g1 s2 . This generalization of giant impact is called a similar-sized collision or SSC. Agnor and Asphaug (2004a) studied collisions between equalsized planetary embryos (r=R) and found that merger is inefficient except when vimp almost equal to vesc. Impact speeds are expected to be higher than this in the late stage of terrestrial planet formation, since the orbits must be planet-crossing. This paved the way to studies (Asphaug et al., 2006) of geophysical and compositional Author's personal copy 200 E. Asphaug / Chemie der Erde 70 (2010) 199–219 evolution in a broader range of scenarios ðr t RÞ. They found that it is common in gravitationally stirred-up populations for planetary embryos somewhat smaller than the largest to dash up against the largest but not accrete. These hit and run collisions dismantle the impactors (r) or catastrophically disrupt them in peculiar ways. It is argued below that many or most of the unaccreted nextlargest bodies (NLBs) surviving the late stage of planet formation bear the scars of one or more hit and run collisions. A remarkable diversity is then predicted for the final collection of NLBs, whether they be Mars and Mercury of the inner solar system, middle-sized members of Saturn’s satellites, Vesta and Psyche in the Main Belt, Quaoar and Haumea and other oddities beyond Neptune, or Earthmass planets in solar systems with super-Earths. Next-largest bodies are lucky to be here, and each is lucky in its own way. Hit-and-run can be as common as accretion, when the characteristic random velocity v1 of a planetesimal swarm (relative to distant circular coplanar orbits) is comparable to the characteristic escape velocity vesc of the largest members of the population. This random velocity is added to the escape velocity, so that spherical planets collide at an impact velocity qffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi ð2Þ vimp ¼ v21 þv2esc When random velocity v1 =vesc C0 accretion is efficient, but when v1 vesc hit and run is the most common outcome. The unique petrogenetic outcomes of hit and run collisions, and the predicted diversity of NLBs and the asteroids and meteorites that derive from them, may be indicative of the random velocities that prevail during the dynamical epochs of planet formation, in the earliest stages corresponding to the evolution of chondrites and chondrules, and in the late stages that define the characters of finished planets. 1.1. Accretion basics In the classical accretion theory of Safronov (reviewed in Wetherill, 1980) the random velocity is related to the escape velocity, regulated by the gravitational stirring, according to Y¼ v2esc 2v21 ð3Þ The Safronov number Y is postuated to be 325 during the course of planetesimal growth (Safronov and Zvjagina, 1969; Safronov, 1972) and closer to Y 122 in the late stage of terrestrial planet formation (Wetherill, 1976). This relation arises from the assumption of planetesimal (gas-free) accretion, with random velocities excited gravitationally by the largest bodies into mutually crossing orbits. Based on N-body numerical experiments, Agnor et al. (1999) and O’Brien et al. (2006) find that vimp ranges from41 to a few times vesc during the late stage of giant impacts, broadly consistent with Wetherill’s result. ffi pffiffiffiffiffiffiffiffiffiffiffiffi The ratio v1 =vesc ¼ 1=2Y depends on the location within the size distribution, since vesc and random velocity both change. The ensemble gravitational drag of small planetesimals reduces the velocity dispersion of the larger embryos, so generally v1 is lower for steeper mass distributions (with greater masses of small particles). If gravitational stirring happens to small and large bodies alike, then smaller bodies encounter one another at higher v1 =vesc , so even if the largest encounters are mostly accretionary (v1 =vesc 0:3, say), colliding bodies half as large will have v1 =vesc 0:6, with outcomes that are mostly hit-and run. This is why hit and run is described below as an edge effect, occurring at the margin of the population. Under dynamically cold conditions (v1 5vesc ) the growth of the largest bodies can run away (Greenberg et al., 1978; Weidenschilling, 2008) since the rate of growth dR/dt increases with R. This is because growing bodies sweep up small planetesimals within an enhanced cross-sectional area that is increased by a gravitational focusing factor Fg ¼ 1 þ2y ¼ 1 þ v2esc v21 ð4Þ accounting for slow planetesimals falling in towards the body. The other scenario, v1 b vesc is sometimes called orderly growth; since there is no focusing all bodies increase in radius at the same rate. But orderly growth assumes perfect sticking during a sweep-up of planetesimals at high random velocity. Perfect sticking can be a very poor assumption when v1 b vesc , and this calls to question whether orderly growth is a valid concept. Planet formation is likely to involve quiescent epochs, and also epochs of moderate random stirring dominated by similar-sized collisions. It seems incontrovertible that moderate random velocities are required during the late stage, since orbits must intersect across increasing distances. Epochs of random stirring are also expected during the first few million years of solar system formation. The severe consequences of planetary dismantling by the mechanism of hit-and-run are likely to be vital to the final bulk chemistry of planets. Planetary growth is after all not just the accumulation of a feeding zone by accretionary events; it is also the record of a comparable or even greater number of nonaccretionary hit-and-runs, each with the capacity to dismantle and segregate a next-largest body’s mantle, core, atmosphere, crust and ocean. 1.2. Collision timescale Collisions involving bodies within a factor of 2–3 in size are extended-source phenomena, distinct in important respects from the point-source collisional phenomena that cause the formation of impact craters (Melosh, 1989). A key difference is that there is no physically important central point in a similar-sized collision—broad regions such as the cores respond in one way, and the colliding mantles respond in another. The outer layers (atmosphere, ocean, crust) respond in yet another. The impact locus as it were is hemispheric or even global in extent. The understanding of impact cratering benefits greatly from the principle of late stage equivalence, a strong form of hydrodynamic similarity whereby the fundamental characteristics of a collision are obtained by geometric (power law) combinations of impactor radius, density and velocity (Holsapple, 1993). In cratering this allows meaningful extrapolations of laboratory results to large geophysical scales. Hydrodynamical similarity applies to SSCs, but not the cratering concept of an impact locus. A second major distinction between similar sized collisions and impact cratering is that the contact and compression timescale for an SSC equals the gravity timescale. The smaller planet is deformed mechanically (compressed and sheared) by its abrupt deceleration against the target, while it is deformed gravitationally. Its fate, and the outcome of the collision, may depend upon the inter-dominance of self-gravitational instability and shear instability. The deceleration and deformation of the projectile in a head-on collision occurs on a timescale tcoll ¼ 2r=vimp ð5Þ where vimp is the collisional speed at the time of contact. Because vimp 1 to a few times vesc, the collisional timescale for SSCs is tcoll r=vesc . By comparison, the self-gravitational timescale is pffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi tgrav ¼ 3p=Gr ð6Þ where the density r ¼ M= 43 pR3 ¼ m= 43 pr 3 assuming uniform bodies. This is the time for a sphere of uniform-density matter to orbit itself. Because r R for similar-sized bodies, Author's personal copy E. Asphaug / Chemie der Erde 70 (2010) 199–219 pffiffiffiffiffiffiffiffiffiffiffiffi pffiffiffiffiffiffiffi vesc GM=r pffiffiffiffiffiffiffi r Gr and thus the collisional timescale tcoll 1= Gr tgrav . This confluence of gravitational and impact deformational timescales contributes to the ‘‘lava lamp’’ like quality noticed in movies of giant impact simulations, with collisional deformation countered by gravitational restitution. 1.3. Fate of the bullet In planetary impact cratering the discrete fate of the projectile is only of significance for the most oblique angles of incidence (Pierazzo and Melosh, 2000). For SSCs the fate of the bullet is of principal consequence, even for moderate impact angles close to 301 from normal. This gives rise to a third important distinction between SSCs and impact cratering: for typical geometries, only a fraction of the colliding matter intersects. For impact velocities greater than about 1.2vesc, depending on mass ratio g ¼ m=M, the rest goes sailing on, and the abrupt shears and unloading stresses unleash a host of planetary processes, some rather novel to consider. Taken together, these distinctions point to the existence of a broad range of collisions, with physical outcomes between those of tidal collisions like comet Shoemaker-Levy 9 which disrupted near Jupiter in 1992 (Asphaug and Benz, 1994); and planetary-scale impact cratering events (e.g. Marinova et al., 2008; Nimmo et al., 2008), with an associated diversity of cosmochemical and planetological outcomes. By far the best studied archetype of a similar-sized collision is the giant impact that has been proposed for the origin of the Moon (Hartmann and Davis, 1975). In the latest studies of this scenario, the projectile gets dismantled (literally) by gravitational and mechanical shears and instabilities into two components, its core which merges with the center of the Earth, and its mantle which interplays with Earth’s outer mantle to form a protolunar disk of several lunar masses (e.g. Stevenson, 1987; Benz et al., 1989; Cameron and Benz, 1991; Canup and Asphaug, 2001). This fractionation of the bulk Moon from the bulk Earth, forming a new minor planet (bound as a satellite) lacking in iron and volatiles, illustrates how SSCs can leave their permanent and formative imprint upon unaccreted next-largest bodies. Giant impacts such as the Moon’s formation are high-energy end members of SSCs occurring late in planet formation, when planets are large and vesc pR is large. The phenomenon can scale down to smaller colliding pairs, impacting at correspondingly slower velocity, at earlier stages of planetary formation. For instance, two molten planetesimals colliding during the first 1 Ma at low random velocity (vimp vesc 100 m=s) might look like the Moon-forming giant impact, and take place on the same timescale tgrav . As for solidified planetesimals, for instance cold chondritic asteroids or solidified differentiated embryos, the outcome of a hit-and-run can involve bulk textural changes, including energetic shearing and brecciation. The shear stress in a tidal collision exceeds the strength and internal friction of rocky or icy bodies larger than 100 km, or even smaller if the disruptive effect of a grazing blow is considered. Changes with scale are considered in detail below. 2. Similar sized collisions Most of the colliding mass contributing to the formation of a planet comes by way of the several largest impacts, bodies within an order of magnitude in mass and a factor of a few in size that have been stirred up gravitationally into planet-crossing orbits. During the earliest stages of terrestrial planet formation most of the mass is in small particulates: crystals and amorphous phases of dust and ice grow into clusters, and these into nuggets that one 201 might call planetesimals, which go on to sweep up the smaller bodies in a runaway. This phase is known from chemical, dynamical and astronomical evidence (Meyer et al., 2008) to end early on, although the transition from dust to planetesimals is a strongly debated topic. Cuzzi et al. (2001, 2008) and Johansen et al. (2007) have shown that turbulence can randomly initiate the concentration of small particles into dense clusters that then ride in pack through the gas and dust, resisting further disruption until they contract gravitationally, or through dissipation and sticking, into sizable planetesimals. These mechanisms might make it possible for large asteroid-sized bodies to bypass hierarchical growth and accrete directly out of the planetesimal swarm. Morbidelli et al. (2009) propose on this basis that asteroids were ‘‘born big’’ to explain the apparent factor of 4 overabundance of 100 km asteroids in the present Main Belt relative to a power law. If so, then after the gas and dust have cleared accretion is mostly a matter of similar-sized collisions. Even in the case of hierarchical growth, and a power law distribution of sizes, most of the mass that collides during planet formation interacts at the large end of the feeding chain, with Mars-mass bodies colliding into Earth-mass bodies, and lunarmass bodies into Mars-mass bodies, and so on. Consider a differential size distribution nðrÞpr a ð7Þ where n =dN/dr and N(r) is the cumulative number of planetesimals larger than radius r. In the case a ¼ 4 there is equal mass in equal logarithmic bins, i.e. equal mass in bodies hundreds of km diameter as in bodies meters in diameter. For a comminuted (ground-down) population obeying size-independent fragmentation physics, the theoretically derived equilibrium value is a ¼ 3:5 (Dohnanyi, 1969). But observed planetesimal size distributions are shallower, with the mass in the largest bodies. In the Main Belt the four largest asteroids, within a factor of 2 in diameter, account for half the total mass. Main Belt asteroids trend with a 223, varying with size and sub-population. Recentlydisrupted comet groups and the comet population as a whole appear to have a 1:7 (see Weissman et al., 2004). For planetforming planetesimals, gravitational focusing and oligarchic sweep up of feeding zones shifts the mass further into larger sizes (Kokubo and Ida, 1998). Thus for characteristic minor planet and small body populations, and embryonic populations, most of the mass—and hence most of the colliding mass—is found in the handful of largest and next-largest bodies, whether they are born big or become big. 2.1. Colliding pairs In their studies of the evolving Main Belt asteroid size distribution Bottke et al. (2005) and Morbidelli et al. (2009) use a statistical code to follow the erosional and disruptive evolution of candidate primordial Main Belts, to see which ancestral size distributions could have evolved to the population now observed. Their models consider impactors up to the size of a given target, but no larger—a seemingly obvious choice given that small asteroids are usually demolished by smaller members of the population; among small bodies the random velocities are typically orders of magnitude faster than their escape velocities. Indeed, demolition by an equal sized body seems exotic, let alone by a larger body. But for the largest asteroids, even at modern solar system high velocities, the impactors required to disrupt them by traditional means can be as big as they are—or larger. Fig. 1 shows a differentiated planet 500 km diameter, consisting of 30 wt% iron and 70 wt% rock, impacted by a 200 km diameter rocky asteroid at vimp ¼ 10 km=s (top four panels) and 5 km/s (bottom two panels), Author's personal copy 202 E. Asphaug / Chemie der Erde 70 (2010) 199–219 themselves, a scenario consistent with the Main Belt models by Chambers and Wetherill (2001), Petit et al. (2001), and O’Brien et al. (2007). In a scenario drawn from the simulations reviewed below, a dozen 1002200 km diameter asteroids might result from the hit-and-run breakup of a single Vesta-sized asteroid that collided at a typical impact angle and at velocity comparable to vesc, into a long-gone (eventually scattered or accreted) Moon-sized world. Returning to the question of the apparent excess of 100 km bodies in the Main Belt, it may be important to consider the hit-and-run breakups of next-largest bodies that are torn into chains by impacts into the largest. If the collisional physics works out then the mass budget is amenable, since the broad excess of 100 km diameter asteroids appears to be offset by a deficit of 300–400 km diameter asteroids. 2.2. Growing planets Fig. 1. Differentiated planetesimals and embryos are difficult to disrupt by impact at expected velocities. Here a Vesta-type (500 km differentiated) asteroid is struck by a 200 km diameter rocky body at 10 km/s (top four frames) and at 5 km/s (bottom four frames). Simulations by C. Agnor (Asphaug and Agnor, 2005). The slower impact, at a velocity typical of contemporary Main Belt collisions, is vimp 15vesc and removes the top third of the mantle. The 10 km/s impact, at 30vesc , exposes some core iron to the surface but leaves the bottom third of the mantle bound to the core. This suite of simulations was to study the problem of liberating core material from a differentiated large asteroid; each case is for the most probable impact angle y ¼ 451. Snapshots for vimp ¼ 10 km=s are plotted before and at t= 120, 390, and 12,000 s after contact in the top four frames, and for vimp ¼ 5 km=s at t= 390 and 12,000 s in the bottom frames. The results deepen the quandary of how Vesta, which retains a thick basaltic crust, did so while dozens of other differentiated asteroids were disrupted to their core. If would seem to have dodged quite a fusillade. However, the results lead us to contemplate impactors larger than the target, turning the problem on its head and causing us to leave the target-centric frame of reference behind. in both cases at the most probable impact angle y ¼ 451 (from Asphaug and Agnor, 2005). The 10 km/s impact is 223 times the velocity typical of modern Main Belt collisions, and 30 times the mutual escape velocity of the pair. But this barely does the job of leaving half the mass behind (the definition of catastrophic disruption) and only exposes some bits of core material. The 5 km/s impact, at a more typical velocity, but still 15vesc , blasts off the outer layer but leaves the mantle reasonably intact. Based on this and other modeling (e.g. Scott et al., 2001) it appears that once planetesimals grow large, they become difficult if not impossible to disrupt. This would present a big problem, since meteorites show evidence for the cataclysmic disruption of numerous asteroid parent bodies that were at least several hundreds of km in diameter (e.g. Keil et al., 1994; Yang et al., 2007). What is required is either a very energetically excited population of Main Belt precursor bodies, with v1 =vesc ]30, that is Yu103 , yet miraculously leaving Vesta’s basaltic crust intact, or else a mechanism for disruption that operates at lower levels of excitation. The process of hit-and-run is capable of causing the catastrophic disruption of objects hundreds of km diameter at the relatively moderate random velocities that are expected. It requires asteroid parent bodies to run into objects larger than A different kind of modeling approach for studying planet formation is to build up rather than break down a primordial population, using accretion codes that apply advanced N-body computational methods to directly integrate the orbits and interactions of planets and asteroids around the Sun and in planet-forming systems. Out of computational necessity these codes assume the simplest collisional physics—the perfect merger—in order to facilitate precise dynamical tracking over millions of years, with collisions = mergers leading to finished planets. Fragmentation can be modeled in such codes, but the debris are impossible to integrate much further in time as discrete objects. Planets of mass M, m and radius R, r are assumed to stick when they hit, forming a larger sphere of mass M+ m that conserves linear and angular momentum. Encounters are treated as perfectly elastic gravitational encounters (no mass transfer and no dissipation of energy) if the impact parameter b 4 R þr, and as perfectly inelastic mergers if br R þr, for which case accretion efficiency x ¼ 1 as defined below. Even with these simplifications, only a few hundred to a thousand planetary bodies can be integrated, since the precise treatment of close encounters slows down the calculation with the square of the number of embryos being tracked. And so a broad size range is not allowed if one follows a physically reasonable size distribution. This means that every collision treated explicitly in these models is similar-sized. As a result, efficient merger is not generally a good assumption. The assumption of perfect merger has been found to bestow upon planets a capacity for arbitrarily large spin angular momentum. The impactor’s angular momentum relative to the ! target center of mass is m v ~ b, where ~ b is the impact parameter ! and m v the momentum, and ~ v the relative velocity. Agnor et al. (1999) tracked angular momentum during terrestrial planetforming N-body calculations and found that finished planets in such simulations spin up to rotation periods as short as 1–2 h. This can exceed dynamical stability (Chandrasekhar, 1969). Moreover, such rapid spins would have to be slowed down to present-day rotations by some mechanism, such as loss of a large satellite, or spin–orbit coupling with another planet or its core; see Kaula (1990) in the context of Earth and Venus. The solution appears to be that fast and/or grazing collisions do not contribute much to accretion; this limits the accumulation of spin. How fast, and how grazing, depends on the collisional physics and can be reliably determined using self-gravitating particle-based or other kinds of hydrocode simulations. Perfect sticking is a reliable assumption in the context of mass evolution only when random velocities are slow in comparison to vesc. (The Moon formed at low v1 =vesc , thus ‘‘sticking’’ may not be Author's personal copy E. Asphaug / Chemie der Erde 70 (2010) 199–219 203 quite the right word.) Dynamical friction of disk planetesimals acting upon the embryos (O’Brien et al., 2006) are likely to reduce their eccentricities and inclinations compared to those reported by Agnor et al. (1999) and others. As mentioned, in the earliest stages of growth quiescent encounters were probably the norm, although turbulence and gravitational stirring by initial embryos may excite planetesimals into relatively high random velocities before the dust has cleared. In order to have planetary encounters at all in the late stage, when orbits are increasingly well separated, random velocities must be rather high. If the epochs of planet formation can be discerned dynamically, then they can probably be discerned cosmochemically owing to the dramatically different character of low, medium, and high velocity SSCs, as described in Section 2.7. 2.3. Scale invariance Scale invariance applies to SSCs in the limit of incompressible, self-gravitating inviscid fluid planets. Two 100 m diameter incompressible spheres colliding at vimp ¼ 30 cm=s (a few their vesc) are indistinguishable from two 1000 km spheres of the same density colliding at vimp ¼ 30 km=s, when the velocities are scaled to vesc and distances are scaled to R. Scale-invariance thus provides first-order physical insight rather than a fast rule. It allows us to define this class of planetary collisions (SSCs) where the impactor and target are of similar size, and where the random velocity v1 is similar to the escape velocity vesc. Planets are compressible, and rheologically and thermodynamically complex. For instance, it is quite plausible that silicate melts are to be found deep inside most 100 km diameter or larger early-stage terrestrial bodies. At high pressures these melts are very soluble to water and other volatiles. In contrast, subkilometer bodies are unlikely to retain any appreciable melt or dissolved gas at any stage in their formation or evolution—they are too small to retain heat and too underpressured to retain gas. They may retain ices. These smallest bodies (typical asteroids and comets) are likely to behave as solids or granular solids during collisions, obeying a physics akin to landslides. Large molten planets differentiate with iron in the core, crustforming silicates and volatiles in the exterior, and mantle inbetween. Differentiation increases the gravitational binding energy of the planet making it almost 3 times as difficult to catastrophically disrupt (in terms of impact energy) as an undifferentiated planet of the same composition, based on impact models similar to Fig. 1 (e.g. Benz and Asphaug, 1999). But differentiation also perches the volatiles and silicates at the lowest specific binding energy, making it easier for major impacts and collisions to strip these materials from an otherwise growing planet. Cores and deep mantles become sheltered as was demonstrated in Fig. 1, and so it is truly an enigma that iron should be one of the most common representatives of our meteorite collections. If we restrict ourselves to inviscid, molten, differentiated colliding pairs—astrophysical rather than geological objects—then the most basic assumptions of scale invariance are met. Even then there are important differences arising from powerful shocks and high hydrostatic pressures. Large SSCs (giant impacts) are hypervelocity because the impact velocity vimp exceeds the sound speed of the colliding materials; they are shock-inducing collisions leading to global-scale internal heating and Hugoniot acceleration. Assuming v1 vesc the impact velocity exceeds the sound speed for collisions involving terrestrial planets that are Moon-sized and larger. H2O and CO2 solubility in silicate melts is greatly enhanced at high interior pressures (e.g. Dixon et al., 1988). When a large Fig. 2. Impact geometry in similar-sized collisions, in side view and front view. Only a portion of the impactor intersects any mass of the target, and commonly the center of mass overshoots (defined as grazing). Mantles might intersect, for instance, but not the cores. The smaller body (radius r) is by convention called the impactor, and the larger body (R) the target, but with v1 vesc and r R this is more mechanics than ballistics. Shown are two bodies a factor of 4 different in mass (r ¼ 0:6R, assuming rr ¼ rR ) at the moment of collision, where y ¼ 301 (left) and y ¼ 451 (right). At left the impact parameter b o R; at right b 4R so the center of mass misses the target. From a mechanical point of view, the ‘‘lid’’ ( 30% of the impactor mass at left; 80% at right) gets sheared off as the colliding body is stopped. The non-colliding lid is shaded grey in the plane of collision (top) and in front view (bottom). The mechanics of hit-and-run is much more complex, involving gravitational stresses and torques and shocks and shears. But simple geometry explains why hit-and-run can be prevalent under typical planet-forming conditions. Half of SSCs are more grazing than the case to the right, not counting tidal (b 4 R þ r) collisions. planetary body ‘‘loses its lid’’ (Fig. 2) then its pressurized volatiles (several wt% H2O may be typical) can erupt violently, released over tgrav from hydrostatic pressure P. This pressure is released from a magnitude and over a timescale (kilobars, hours) that is comparable to gas-driven kimberlite eruptions on Earth (Kelley and Wartho, 2000; Porritt and Cas, 2009; Kamenetsky et al., 2007). As shown below in a study of purely tidal collisions, even a tidal (non-impacting) impactor can have its interior pressures lowered by 50% for about an hour, with a rate of pressure release P_ P0 =tgrav r 2 ð8Þ and 20% permanent pressure reduction because of spin-up and mass loss. The pressure release adds V DP to the available specific enthalpy Dh ¼ Du þ PDV þV DP, considered further below, where volumetric expansion PDV occurs especially in the case of bubble formation (Gardner et al., 1999). Most asteroids, by number and perhaps also by mass, are undifferentiated. The effects of SSCs among primitive and undifferentiated populations of smaller bodies may be more subtle than for larger, differentiated bodies for three reasons. One, shock levels will be well below the sound speed if v1 vesc , for objects much smaller than the Moon. Two, the pressure unloading effects just described may be small. Three, surface-stripping and fragmentation may not result in a noticeable change in bulk chemistry or composition since there is no core–mantle segregation, and hence no crust to remove from a mantle, or mantle from core. Nonetheless it is important to keep in mind that similar sized collisions do happen to primitive bodies, and that hit-andrun collisions happen when random velocity is comparable to escape velocity. These collisions would be gravity- and Author's personal copy 204 E. Asphaug / Chemie der Erde 70 (2010) 199–219 shear-dominated, not shock-dominated. These shears can leave their imprint; moreover, while pressure unloading from tens of bars of pressure (the interior of a disrupted 100 km body) might not stimulate global melting or degassing as studied further below, the unbalanced pressure gradients and available enthalpy could trigger volatile migration and hydrous activity in otherwise primitive bodies. 2.4. Collisional geometry In impact cratering, the projectile is rapidly buried into a semiinfinite target and effectively explodes, coupling as a point source without much downrange ballistic motion. The impact angle can be parameterized with good results, as there is little difference to the physics except for the shallowest collisions (Pierazzo and Melosh, 2000). Similar-sized collisions on the other hand are sensitive to impact angle over all ranges of y, simply because a similar-sized impactor does not have semi-infinite mass to bury itself into. Fig. 2 shows how a large fraction of the mass misses the target for any but the most direct hits. Impacts that would not be considered oblique in the context of impact cratering (y 302601) are grazing when it comes to SSCs, in the sense that most of the mass overshoots. The probability of impact at an angle between y and y þ dy by a point mass onto a spherical gravitating target is 12 sin2 y dy, a function that peaks for impact angle y ¼ 451 (Shoemaker, 1962); 451 is also the median impact angle. The impact angle for undeformable colliding spheres is the same as that of a point mass at the impactor center, impacting a virtual sphere of radius R þr, thus Shoemaker’s original argument applies to SSCs. If one defines impact parameter b (Fig. 2) as the offset from the impactor trajectory from the target center of mass at the moment of collision, then p b¼ ffiffiffi ðr þ RÞsiny and the most likely impact parameter is b45 ¼ ðr þRÞ= 2. (Note that b is somewhat larger than the periapse that would be computed for a collisionless encounter, at the moment of periapse when two virtual spheres are intersecting.) For impact cratering (small r/R) the traditional definition of grazing is b= R, where the impactor skims tangential to the target. Abstract this notion so that the threshold for grazing is when the center of mass of the smaller colliding body is tangential to the larger (Fig. 3): R ð9Þ yb ¼ sin1 Rþr For equal sized planets r ¼ R and grazing requires an impact angle that is only 301 from head-on. When r = R/2 grazing occurs for y 4 yb ¼ 421; that is, more than half of all collisions for bodies within an order of magnitude in mass. For small r, the fraction f that is shaded grey in Fig. 2 approaches a step function, corresponding to the fact that impact cratering into a halfspace is all-or-nothing, while for SSCs there is broad gradation over a range of impact angles. That is why their outcomes are so diverse. If two differentiated planets collide, then their cores miss one another entirely for ycore 4sin1 ðrcore =rÞ ð10Þ where the bodies have the same core fraction rcore/r = Rcore/R (Fig. 4). Among terrestrial planets rcore r=2, so for any impact between 301 and 901 the cores miss one another. While this is a simplistic approach to collisions, it soundly predicts that the level of core–core interaction during giant impacts is highly variable, with some events shredding and intermingling mantle materials but not cores, and others merging cores entirely. Idealized assumptions about planetary collisions and their mixing are probably untenable; see Nimmo and Agnor (2006) for modeling and discussion of this issue. Fluid bodies deform during SSCs and are ellipsoidal by the time of impact (e.g. Sridhar and Tremaine, 1992). Shoemaker’s argument for impact angle is no longer valid; impact angle is not well defined and angular momentum goes into torques. Cores interact with the mantles they plow through, which are about twice as massive, and can therefore merge even if not headed right at one another (see the Moon formation models discussed below). Impact trajectory is not a straight line. Mass does not come off as a ‘‘lid’’. And lastly, concerning grazing, there is no abrupt change in the physics between an impact involving a small fraction of the target (b t r þR), and an impact that barely misses (b \ r þR). The discussion of impact angle must be nuanced to account for tidal collisions, for which y is undefined, which may be of great consequence to the impactor especially if the mass ratio g ¼ m=M t 0:1. 2.5. An edge effect Hit-and-run can be thought of as an edge effect pertaining to the planets that are similar in size to the largest, within the factor r=R 13 for which grazing is common. An accreted planet that has grown into one of the largest, has nothing larger to run into. 90 Grazing Impact Angle 80 70 60 50 40 30 0 0.2 0.6 0.4 0.8 1 r/R Fig. 3. The threshold grazing incidence angle yb (Eq. (9)) as a function of relative sizes of the colliding pair r/R. Grazing is defined as the center of mass of the impactor missing the target (Fig. 1). For relative size r=R \ 0:4 most collisions are grazing (yb r 451). Purely tidal (non-impacting) collisions are an important class of grazing collisions (see Fig. 13) but are not included here as y is undefined. Fig. 4. A collision with impact angle greater than yc ¼ sin1 ðrcore =rÞ may have little direct core–core interaction. The core in this case is half the radius, so that ycore ¼ 301. Impacts steeper than ycore will trend towards great core interaction (and mergers for low velocity), while shallower impacts (most of them) might have little core interaction. Author's personal copy E. Asphaug / Chemie der Erde 70 (2010) 199–219 Fig. 5. Similar sized collisions are an edge effect occurring between the largest and the next-largest bodies in a hierarchically accreting size distribution (see text). Here is a plot of cumulative number N versus size r, schematically a power law. The largest and next-largest bodies have mutual collisions v1 vesc . The ratio v1 =vesc increases with 1=r, and so is high (disruptive) towards the left of the plot. Unaccreted NLBs, though still among the ‘‘giants’’ in the context of the late stage, finish their evolution as part of the middle of the pack (Fig. 5). Being among the largest, they are petrologically interesting, potentially thermally active, differentiated, and complex. If they are broken down into smaller ð 100 kmÞ objects early on, their interiors are represented in the final population of asteroidal parent bodies and in the meteorites; if they are not, then their interiors remain forever sheltered, as Vesta’s has been. Collisions with largest bodies occur at v1 vesc as stirred up by those same bodies. Smaller bodies in the population are subject to the same random stirring, and either accrete onto the larger bodies rather efficiently, or else catastrophically disrupt with other small bodies, considering their relatively low binding energy (vimp bvesc ). Thus SSCs as we have defined them do not occur throughout the size distribution, but between the largest and the next-largest for which vimp vesc . Hit-and-run is a third way for planets near the top of the size distribution to evolve and exchange material and momentum during accretionary epochs, in addition to merger (which grows larger planets, and must at some point be dominant) and disruption (which reverses the process of accretion and must become minor for planets to form). While the associated processes of impact shredding may seem exotic, hit-and-run is actually more common than merger or disruption for SSCs at typically stirred-up random velocities. It plays an important and perhaps dominant role in the physical and chemical evolution of the planetary bodies that grow large, but not largest, in terrestrial planet-forming settings. 2.6. Modeling similar-sized collisions Canup and Asphaug (2001) conducted a systematic study of potential Moon-forming collisions, based upon computer simulations using the smooth-particle hydrodynamics (SPH) method pioneered for giant impact studies by Benz et al. (1988), Cameron and Benz (1991) and others. SPH is a Lagrangian method that uses smoothed mass elements (spherical kernel functions) to compute 205 the hydrodynamic and shock stresses and the pressure and gravity accelerations, and to track the trajectory and evolution of matter. We used a simple but appropriate nonlinear equation of state (Tillotson) for iron cores and rocky mantles, and set the random velocity to zero (vimp = vesc) in order to maximize the disk mass while satisfying the constraints of final system angular momentum. The impacts studied were otherwise characteristic of terrestrial planet-forming collisions. In the course of this search for the best case scenario for latestage Moon formation around proto-Earth, we made a few exploratory simulations with v1 40 and found that some of these impacting planets were ‘‘skipping’’ from the target Earth. Indeed, the best case scenario identified for Moon formation turned out to be an impactor which almost, but not quite, skips off (see Fig. 6). A fraction faster and there would have been no Moon, but two planets—one still rather Earth-like, and the other one less massive than before, missing much of its mantle—resembling Mercury, perhaps. Fig. 7 shows frames from two simulations by Agnor and Asphaug (2004a, b) in studies of accretion efficiency and the thermodynamical aspects of SSCs (Asphaug et al., 2006). These are typical of the two main kinds of hit-and-run collisions, one a rebound and the other chain-forming. Planets before the collision are hydrostatic, non-rotating, and start from a separation distance 5Rroche . Impact velocities are vimp ¼ 1:5vesc in (a–c) and vimp ¼ 2vesc in (d–f), corresponding to v1 ¼ 1:1vesc ; 1:7vesc , respectively. The impact angle is 301 in both cases. The first scenario results in widespread mantle removal from the impactor; the scenario is postulated below as a mechanism for Mercury’s mantle loss. The second case results in a chain of bodies the size of the major asteroids, all of them highly diverse in major element abundances (and most of them iron-rich), but each deriving from the same parent body chemistry. Research is flourishing in the area of planet-scale collisional modeling thanks in part to a renewed focus on the formation of Earth-like planets around other stars (e.g. Marcus et al., 2009) and the great strides that have been made in the development of selfgravitational hydrocodes capable of evolving millions of particles, and the computer systems to run them on. Much higher resolution giant impact simulations are now possible including the use of more detailed and accurate equations of state (see e.g. Benz et al., 2007). The greatest challenge may be the accurate modeling of smaller-scale SSCs where gravity is not the only force to be considered; complex effects such as porosity and strength are notoriously challenging to model (Jutzi et al., 2008, 2009). Furthermore we have yet to adequately understand the long term dynamical fate of collisional ejecta—whether it reaccumulates onto the target or onto the unaccreted impactor after many orbits about the Sun, or becomes background disk material, or is lost by solar effects. Moreover, the effect of spin has not been explored systematically for SSCs, or in the context of accretion efficiency; Canup (2008) has made the first inroads in the context of Moon formation. 2.7. Accretion efficiency For gravity-dominated collisions SPH is well suited, even at moderate resolution, to computing the final total bound masses M1 and M2 where M1 is the largest collisional remnant and M2 the second largest. In the limit of a non-collision M1 = M and M2 = m. After a collision the binding energy of all particles is computed with respect to the particle closest to the global potential minimum, which serves as the seed for nucleating the total bound mass of the largest aggregate M1. The binding energy of remaining particles is computed with respect to this new position Author's personal copy 206 E. Asphaug / Chemie der Erde 70 (2010) 199–219 Fig. 6. Hit and almost run. Moon formation in a late stage, low-velocity collision with proto-Earth, in a giant impact scenario modeled by Canup and Asphaug (2001). Color indicates thermal energy. A proto-lunar disk of the appropriate mass, angular momentum and mantle-derived bulk composition forms after a Mars-mass impactor (0:1M , coming from the right) collides at vimp ¼ vesc into a 0:9M body. It first bounces off, as seen in the top four frames, but is now gravitationally bound, and comes back after a few hours to be further shredded by tidal and impact shears. The impactor’s core merges with the proto-Earth’s. Molten and vaporized ejecta from the crusts and mantles of the impactor and target shears out into a protolunar disk of about two lunar masses in this simulation. Shown are times t=0.3, 0.7, 1.4, 1.9, 3.0, 3.9, 5.0, 7.1, 11.6 h after initial contact. Identical simulations at 30% higher impact velocity end with the impactor escaping as a novel planet, a Mercury-like body stripped of its crust and outer mantle. Fig. 7. Hit-and-run is a common outcome when planetary bodies of similar size collide. Shown are frames from 3D SPH simulations using the Tillotson equation of state 1 (from Asphaug et al., 2006). In each case a Mars-mass target is struck by a planet 12 (top) and 10 (bottom) its mass (statistics for these and other simulations are plotted in Fig. 8). The top is a rebounding collision at vimp ¼ 1:5vesc ; the bottom is a chain-forming collision at vimp ¼ 2vesc . Rocky mantle is labeled blue and iron red. Particles are shown in side view before, during, and 3 h after the collision. Blue particles appearing to mix into the target core are a projection effect of particles with the same ðx; yÞ in and out of the page; there is little if any disruption to the target core. and velocity, and the second largest aggregate M2 computed, and so on as allowed by resolution. The accretion efficiency x¼ M1 M m ð11Þ is determined to better than 10% in these simulations, where x ¼ 1 for a perfect merger, M1 =M +m. The determination of M1 is resolution converged using modest ( 3 104 ) numbers of particles. That is, the answer does not change with further increases in resolution. Nor has this basic result been found very sensitive to the equation of state (EOS), provided it is adequate to Author's personal copy E. Asphaug / Chemie der Erde 70 (2010) 199–219 model shock acceleration. The Tillotson EOS and the more sophisticated ANEOS and SESAME EOS give very similar results for this basic quantity of a similar-sized collision. Modeling Moon formation using the same computational tools is a much bolder endeavor than modeling x. Only a few percent of the collisional ejecta end up in a proto-lunar orbit, as satisfied only by a narrow range of ejection velocities between pffiffiffiffiffiffiffiffiffiffiffiffiffi vorb and vesc, where vorb ¼ GM=a and a is the radius of the protolunar disk that forms outside the corotation radius. The dynamics must then be evolved by the code for at least one orbital time in response to very near field gravitational torques. The longer timescale and higher required precision result in a sensitivity to the equation of state (explored in Canup, 2004) and to radiative evolution (Stevenson, 1987) which is not included in these SPH models. Accretion efficiency is plotted in Fig. 8 as a function of the random velocity v1 (Eq. (2)) for Mars-mass planets (M ¼ 0:1M ) struck by impactors m ¼ 0:01M ; 0:05M ; 0:1M (mass ratio g ¼ m=M ¼ 0:1; 0:5; 1:0) at impact velocities vesc rvimp r 3vesc . The data are derived from 144 simulations performed by Agnor and Asphaug (2004a, b) including the two shown above in Fig. 7. The results for x appear on the basis of other simulations to be scale invariant within 10% for larger and smaller differentiated terrestrial planetary masses (approximately Vesta sized to super-Earth sized) so the plot can be studied as a general result for terrestrial planet formation. The Moon-forming giant impact scenario favored by Canup and Asphaug (2001) plots near the upper left red triangle. In all these simulations the spatial resolution is 30,000 particles, and the iron:silicate mass ratio is 30:70 as a core and mantle. Planets are hydrostatic and non-rotating prior to collision, and are placed initially at 5Rroche to allow the pre-impact tidal strains and torques to develop. 207 Ignoring purely gravitational (tidal) collisions (Fig. 13 below), for which y is undefined, the impact angles 301, 451, 601, 901 each represent 14 of the impact probability of collisions, dPðyÞ ¼ 12sin2 y dy, with 01 being head-on. The velocity range covers the expected range of collisional velocities during late-stage planet formation. However, the simulations between 0 and 0.7vesc are rather coarsely spaced given the sensitivity of outcomes in this range, and need to be filled in with further simulations to better understand the transition from accretion to hit-and-run behavior. Also, the range of mass ratio needs to be extended to g 0:03 in order to cover all similar-sized collisions; these results are for g ¼ 1, 0.5, 0.1. A finer resolution in impact angle would better reveal the nature of this transition as well. But the initial observation can be made, that there are four main branches of similar-sized collisions: 1. Efficient accretion is the common occurrence for random velocities lower than about 0.6vesc. Damped populations accrete efficiently. 2. Partial accretion is common throughout the random velocity range 0:722vesc . Mergers are inefficient at high velocity. Only direct hits (01, 301) are accretionary at all for random velocities greater than about 0.8vesc. 3. Hit and run is prevalent for the velocity range 0:7vesc t v1 t2:5vesc , i.e. 1:2vesc tvimp t 2:7vesc . The clustering around x ¼ 0 corresponds to impactors rebounding with little net mass contribution to the target, or little erosion. 4. Erosion and disruption occur for random velocities greater than 2:5vesc . These tend to destroy the smaller body (most is not accreted) and erode the larger. Catastrophic disruption, traditionally defined as M1 = M/2, requires collisions at velocities far to the right of this plot (xcat ¼ 12M=m). The distinction between partial accretion and hit-and-run owes to a remarkable sensitivity to impact angle; this shows in the figure Fig. 8. Accretion efficiency x (Eq. (11)) for colliding planets as a function of random velocity, for colliding mass ratios g ¼ 0:1, 0.5, 1.0 and for impact angles 01 (head-on), 301, 451 and 601. Data are from smooth-particle hydrocode impact simulations by Agnor and Asphaug (2004a, b) that assumed differentiated targets and impactors, 30 wt% iron core and 70 wt% rocky mantle. Each angle represents 14 the probability interval of collisions. Impact velocity vimp ranges from vesc to 3vesc ; the normalized random qffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi pffiffiffiffiffiffiffiffiffiffiffiffiffi velocity v1 =vesc ¼ ðvimp =vesc Þ2 1 ¼ 1=2Y is the abscissa in this plot. The simulations reveal an abrupt transition from efficient accretion (x 1) to hit-and-run (x 0) around Safronov number Y 1 (labeled at top; Eq. (3)), corresponding to vimp 1:2vesc and v1 0:7vesc . For faster impacts, half of the collisions studied (those Z 451) are effectively collisionless from the point of view of bulk mass accumulation. Author's personal copy E. Asphaug / Chemie der Erde 70 (2010) 199–219 as a segregation by plotted color, where red and green dominate the hit-and-run line xhr 0 ð12Þ For random velocities v1 \ 0:7vesc half of the collisions (those Z451) are effectively collisionless from the point of view of bulk mass accumulation. Even for relatively normal impact angles (301) the influence of grazing is pronounced. This leads to the most striking aspect of the plot, which is the abrupt jump to the hit-and-run line with increasing impact velocity and impact angle. For a broad and significant range of impact angles and velocities there is little net mass contribution or removal from the target. 2.8. Prevalence of hit-and-run Hit-and-run is prevalent in systems that are moderately gravitationally excited and less so in systems that are not. A simple framework model is developed to trace the occurrences of hit-and-run on the path to planet formation. The model is not dynamical: planetesimals are given an initial random mass (following a power law, Eq. (7)) and allowed to grow through randomly selected pairwise collisions. The total starting mass is a constant. If a colliding pair is within a factor of 30 in relative mass (based on Fig. 3), and one of them is within a factor of 30 in mass of the largest body in the simulation (so that vesc v1 ), then it is a similar-sized collision as defined above. Each SSC has a probability of hit-and-run (x ¼ 0) or merger (x ¼ 1). If a merger, then the smaller body goes away and the largest becomes the sum of the masses, and carries a mass-averaged tally of the number of hit-and-run occurrences which starts off at 0 for all bodies. Hit and run does not change either body in the model, but increments the hit-and-run tally of the smaller by 1. Large colliding pairs with 1 mass ratio g o 30 are presumed to be efficiently accreted. Small 1 colliding pairs, however, in which both masses are smaller than 30 the largest in the simulation, have vesc 5v1 and so the bodies are regarded as disrupted and removed from the population. Pairwise collisions proceed, under the assumption of constant Safronov number, until the final number of bodies has been reduced to Nfinal. Results are plotted in Fig. 9 for a moderately excited population (v1 vesc ) for which the probability of hit-and-run is about 50%. Hit-and-run happens commonly to most of the nextlargest bodies in a population in that case. If one mass-averages the history of hit-and-run in the assembly of the largest final bodies, then it is important to the largest as well. This samplingwith-replacement result is not surprising to anyone familiar with statistics, but it may lead to a revised thinking as to how we interpret planets and their acquisition and retention of mantles. The scenario beginning with Ninit ¼ 10; 000 ends up with a population of largest and next-largest objects (black diamonds) having had 4 or 5 hit and runs each; the largest are rather homogeneous in terms of mass and hit-and-run tally. The ‘‘late stage’’ scenario beginning with Ninit =100 allows two bodies to avoid hit and run by chance. The two largest are again similar in size and tally, and accreted from bodies that had 1 hit and run on average. The NLBs in this case are a very diverse group, some having no hit and runs and others having 2 or 3. Much of the material stripped off by hit and run early on may end up back in the disk, to be accreted later. It is a challenging study, how to model disk replenishment during N-body integrations. Nevertheless, a more physical study than the above is possible, regarding the hit-and-run characteristics of accretion. N-body integrations could import the outcomes from SPH codes, allowing the dynamics (including spin) of growing/eroding/ disrupting planets to change with every impact. With the advent Hit and Run Occurrences for v∞∼vesc Hit and Run Occurrences (mass averaged) 208 10 10,000 -> 10 100 -> 10 1 1000 10000 100000 Final Planet Mass (normalized) Fig. 9. Accretion including the occurrence of hit-and-run is modeled schematically as a collection of Ninit planets growing by random pairwise collisions (see text) into the 10 final planets that are plotted. Hit and run, accretion and disruption occur in approximate concordance with Fig. 8. Here the assumption is a moderately stirred up population (v1 ¼ vesc ) so the probability of hit and run is 50%. The y-axis shows the number of hit and run events each final body has experienced (mass averaging the hit-and-run tally of accreting bodies) by the end of accretion. The runs start with either Ninit ¼ 10; 000 or 100 bodies, of the same total mass. of commodity GPU computing it is not far-fetched to imagine running a fairly quick SPH simulation at every detected collision. Adding mass back to the disk, providing drag, could perhaps be done by tracking millions of collisionless planetesimals. But the problem is extremely complex. The size-frequency distribution of the disk planetesimals changes the random velocities of the embryos, through stirring damped by dynamical friction, while the random velocities of the embryos changes the size distribution of planetesimals by changing the collisional physics. 2.9. Accreted and unaccreted Two bodies that come into close proximity once in their orbits about the Sun, at the moderate random velocities considered here, are likely to do so again unless their orbits are externally perturbed. Thus, bodies involved in a hit and run collision are expected to come back again to try once more. Given a few tries, accretion is likely. Accretion must be overall efficient for it is known from isotopic age dating (e.g. Yin et al., 2002) that accretion won out after a few 10 Ma, and terrestrial planet formation effectively ended in our solar system, in concordance with N-body simulations that assume perfect merger. Planetary bodies on colliding orbits, for the most part, eventually accrete. But the surviving next-largest bodies that did not accrete onto the largest bodies are not ‘‘the most part’’. There is a severe selection among the surviving NLBs. As with an epic military campaign in which nearly all of the soldiers have fallen, the survivors have tales of miraculous good fortune to recount. Those planets and planetesimals that participated in accretion, but by a relatively small chance of dynamics neither merged nor were scattered, thus remain behind as a rather exotic population of NLBs. Planet growth proceeds apace for the largest, in the sense that merger happens when it happens, and non-merger does not grossly affect their mass (x 0) except at the highest relative velocities. Even if it takes several tries, one can to first order ignore a few unsuccessful attempts at accretion. There is some shock and mechanical processing and impact erosion of the target, but not much loss or exchange of matter compared to the devastation that happens to the bounced-off impactors. Author's personal copy E. Asphaug / Chemie der Erde 70 (2010) 199–219 The evolutionary tendency is towards a compositional change that discriminates, over time, the largest from the next-largest bodies. With each non-accretionary event the NLBs get stripped of their outer layers, becoming increasingly iron-rich and volatilepoor. If it takes an NLB several collisions to accrete, by the time it does merge it will tend to increase the iron fraction in the largest. Its stripped outer silicates and volatiles go back into the disk; any discrete parcels of this stripped material have similar dynamical parameters and future encounters are likely with either of the colliding pair, perhaps favoring the larger on account of its greater gravitational cross-section. If so then the largest bodies can rob, over time, the exterior materials from the NLBs, leading to a compositional dichotomy between the accreted and the unaccreted. The late stage of planet formation ends with planets achieving stable orbits. Remnants of these final collisions are trapped and herded into relatively stable dynamical regions (Morbidelli and Moons, 1993), providing a snapshot in our solar system of how terrestrial planet formation all ended some 4.6 billion years ago, punctuated by dynamical hiccups (e.g. Chambers, 2007; Gomes et al., 2005). By the very nature of the late stage, most of the colliding matter is in the largest sizes; nearly all of the debris that is produced is the result of similar sized collisions, from megacratering events (Marinova et al., 2008) to the unaccreted strands and clumps of hit-and-run debris. The Main Belt should thus be replete with mantle- and crustal-derived rocks from collisions between differentiated late-stage embryos (the spray of debris colored blue in the simulations of Fig. 7). However, stony achondrite meteorites are uncommon compared to the great diversity of irons, which are presumably the core relics, and relatively few are unequivocally mantle-derived. As for spectroscopically characterized asteroids, the vast majority are undifferentiated; if there is much mantle rock in the Main Belt it is hiding. Burbine et al. (1996) considered this puzzle and hypothesized that because mantle rock is friable, once liberated from a parent body it rapidly degrades into sub-millimeter sizes and is swept away by Poynting–Robertson drag or the solar wind, or solar radiation pressure. Iron, being more resilient, survives to produce meteorites. Asphaug et al. (2006) argue that the debris may begin as mantle rock but undergo petrogenic transformation during release from hydrostatic pressure, or if solid, be fragmented in situ by the unloading stresses. 3. Departures from scale invariance Most impact simulations are based on fully compressible fluid dynamics computations including the calculation of shocks and the reasonably accurate calculation of the equation of state relations Pðr; uÞ where P is pressure and r; u are density and internal energy of the represented material. Simulations using the same SPH code and Tillotson EOS indicate approximate scale invariance for equivalent impacts involving planets ranging from Vesta-sized to Earth-sized, when the velocities are scaled to vesc. Using a different SPH code and EOS model (and minor differences in setup) Marcus et al. (2009) reproduce part of Fig. 8 for superEarth-sized planets, and obtain very similar results at a much larger scale. But similarity in computational results is not proof of scale invariance in nature. We consider these invariances by approximating some of the geophysical complexities, considering strength at small scales, enthalpy at large scales, and viscosity inbetween. In addition one must acknowledge that impact physics itself changes fundamentally as one transitions from hypersonic collisions (much faster than the sound speed in the rock, the largest events) to subsonic small-scale events, the 209 transition velocity being a few km/s for rocky bodies but much slower for uncompacted bodies. Along these lines one can identify four scenarios to explore for departure from scale invariance as one transitions from large, differentiated, fluid planets (the easiest to model) to SSCs involving smaller colliding pairs. Rheology: Brittle mechanical strength is size and rate variant (Grady and Kipp, 1985; Melosh et al., 1992), and is not well understood for the tens of m/s velocities that may be common among colliding planetesimals. For deformation on the timescale tgrav of a similar sized collision, large bodies are likely to be dominated by viscous rather than brittle deformation, first because they are massive—their interior pressures far exceed the stresses associated with the failure of elastic solids—and because they retain heat and are more likely to remain ductile. Differentiation: Closely related to the thermal state, or past thermal state, is the transition with increasing size towards differentiated internal structures. Colliding bodies whose iron has segregated to the center, and whose atmosphere and volatile condensates (oceans) have migrated to the exterior, behave differently than undifferentiated colliding spheres. Impacts preferentially remove the lower-density outer layers which receive the brunt of the impact energy. Impedance mismatch at the core–mantle boundary (Asphaug, 1997) may also enhance the velocity of ejected materials from the outer layers. These effects change the physics with scale, and work to segregate planetary materials. Shocks: Because impact velocity scales approximately with the size of the colliding bodies (vesc in m/s is equal to R in km, for a sphere of uniform density 1.9 g cm 3) there is a tendency for SSCs involving \1000 km bodies to produce shocks, at impact velocities exceeding the sound speed of their material. For giant impacts at tens of km/s shocks can induce global melting, while for primary accretion the collisions may be only a few m/s. Subsonic impacts may only result in damage (if solid) or in compaction or shear bulking (if granular; see e.g. Schäfer et al., 2007), or splashing if liquid. Shocks are less important for very grazing SSCs in which the bulk of the matter does not intersect. Unloading: The lithostatic overburden pressure of a nonrotating incompressible planet of radius r is PðaÞ ¼ 23 pGr2 ðr 2 a2 Þ where a is the distance from the center. The characteristic pressure P0 ¼ Gr2 r 2 is released to a much lower value during the collision timescale tcoll . The effect of pressure release can be subtle for small bodies—it may have been expressed in the vigorous dust production of comet Shoemaker-Levy 9 after its tidal disruption by Jupiter (Hahn and Rettig, 2000)—and it can be hugely important for large bodies. If one thinks of planetary disruption as an enthalpy-conserving event, and ignores shocks, then the change in specific enthalpy goes as r2. Moon-sized and larger bodies have potential for widespread eruptive degassing and hydrothermal action at global scales, even in response to purely gravitational (tidal) collisions. Based on Earth analogues, pressure release melting and plinian-type magmatic responses might occur at global scales. 3.1. Rheology Rheology pertains to how geologic materials deform and flow. The simplest planetary rheology invokes a strength (that is, a cohesion or yield stress, which could be zero) beyond which material deforms, for instance as a viscous fluid. Strength and flow are quite complicated, but a simple approach is suitable here. 3.1.1. Strength Strength is scale variant primarily because large objects have bigger flaws. If one thinks of an object’s volume as sampling a Author's personal copy 210 E. Asphaug / Chemie der Erde 70 (2010) 199–219 probability distribution of possible flaws (Weibull, 1939) then static tensile strength S expressed as the weakest flaw in a volume, decreases approximately with size to a power S r 3=m where m 629 for typical rocks (Grady and Kipp, 1985). This leads to large asteroids requiring much less specific energy to catastrophically fragment than small ones, whether by tidal or by collisional stress. In addition strength is rate variant for the same underlying reasons (see Melosh et al., 1992), materials being stronger in proportion to the strain rate. It is worth noting as an aside that ejection velocity vej from a rocky target scales approximately with the square root of tensile strength, Y v2ej , because strength is a specific energy. Thus, the strength of an asteroid’s rock type probably biases which meteorites we look at, by sending the strong ones on the quickest journeys to Earth, where in turn they are most likely to survive the voyage through space, and atmospheric entry and terrestrial residence prior to discovery and curation. Catastrophic disruption requires acceleration of the fragmented materials to escape velocity. As Fig. 1 showed, large bodies are tightly bound and difficult to disrupt even if they have no strength. The corollary is that rubble piles are ubiquitous for asteroids larger than some size, believed to be about 300 m diameter (Benz and Asphaug, 1999; Holsapple et al., 2002) since global fragmentation energy is lower than binding energy. Beyond some further size, perhaps a few 100 km diameter, selfgravity and deformation begins to compactify the rubble into a coherent body (perhaps with the assistance of impact cratering) as the central pressure exceeds the compaction strength of rubble, and as thermal deformation and melting become important. Cohesion, as the threshold for shear deformation, has been studied in the context of planetary tidal disruption. Jeffreys (1947) analyzed the gravitational disruption of planetesimals passing inside the Roche limit of Earth, treating them not as fluid bodies but as elastic solids subject to a deformational stress. Because the tidal stress increases with r2, bodies smaller than a certain size do not fragment. Jeffreys found that a monolithic rocky asteroid smaller than a few 100 km diameter survives a grazing encounter with Earth. This assumes that tensile strength is not size-varying; a Weibull distribution of flaws pushes the transition to smaller sizes, between fragmenting and nonfragmenting interlopers, and more abruptly. As with most pioneering research, Jeffreys’ specific result was eventually rendered somewhat moot, in this case by the recognition over the past decade that asteroids of that size are likely to be rubble piles. Resistance to deformation for rubble pile objects is not measured by tensile strength, but is a complicated granular rheology that depends on the overburden pressure and the total stress condition. Small monolithic bodies might not come apart by tides, but rubble piles might (Richardson et al., 1998). Consider the imprint of tidally disrupted comets upon Jupiter’s satellites—or rather, the unexpected absence of such imprints from disrupted parent bodies smaller than about 800 m (Schenk et al., 1996; see Fig. 10). There are more than a dozen larger records of tidally disrupted comets, and none smaller. It may be that Jupiter-family comets are structurally competent at some small value but that once their cohesion is exceeded they disaggregate and behave rather like a fluid (Asphaug and Benz, 1996). The abrupt transition from solid to fluidized behavior is a common aspect of granular materials, and may be pronounced under microgravity conditions. The structural competency of Jupiter-family comets (JFCs) overall appears to be comparable to the jovian tidal stress, which across such a small body is not much greater than that of a dry snowball. In modern times comet Shoemaker-Levy 9 disrupted at Jupiter, an event matched by a 1.6 km diameter progenitor of bulk density 0.6 g cm 3 (Asphaug Fig. 10. Tidal disruption remnant imprinted as a chain of craters on Jupiter’s satellite Ganymede, imaged in 1997 by the Galileo orbiter (see Schenk et al., 1996). North is up; sun is from left. This is Enki catena, about 160 km long, produced when a comet broke apart in a near-parabolic tidal collision with Jupiter and hit Ganymede on the way out. Its dozen equant fragments are indicative of gravitational breakup of a fluidized body (Asphaug and Benz, 1996). Galileo SSI/ NASA. and Benz, 1994) and strength 100 dyn cm2 disrupting as a fluid body during a few hours inside the Roche limit. If small planetesimals behave somewhat as self-gravitating granular fluids during randomly stirred planetary encounters, then perhaps SSCs are dynamically similar from scales ranging from giant impacts to planetesimals the size of small hills. Detailed numerical models (Schäfer et al., 2007) and laboratory experiments (Wurm and Blum, 2006; Dominik et al., 2007) of colliding aggregate bodies give various results, not always consistent, showing how crushable or fractal solids can behave in unexpected ways. Polyhedral rubble pile models by Korycansky and Asphaug (2006) illustrate the transition from individual to ensemble behavior and the phenomenon of granular collapse in a self-gravitating system. There is much to be learned about this ‘‘mesoscale’’ of accretion, where there is no well-understood characteristic stress or characteristic size. 3.1.2. Viscosity If colliding planets are large enough, or molten, then strength and cohesion are effectively zero and the bodies are compact. The above complexities go away and what remain are the equation of state (EOS) and the deformation rheology. Concerning the latter, the easiest approach is to consider a linear Newtonian viscosity; if the planet resists deformational shears on the collision timescale then it will not disrupt. Newtonian viscosity is the ratio of stress to the strain rate Z ¼ s=e_ ð13Þ A similar sized pcollision ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi takes place over the gravitational timescale tgrav ¼ 3p=Gr (Eq. (6)), a couple of hours for density corresponding to terrestrial planet-forming materials. The strain rate of deformation is then e_ ¼ e=tgrav ð14Þ for some shear strain e. If the stress is primarily gravitational (tidal or shear disruption against self-gravity) then the characteristic stress is s P0 Gr2 r2 where r is the radius of the disrupted body. ð15Þ Author's personal copy E. Asphaug / Chemie der Erde 70 (2010) 199–219 211 shocks or damaging stress waves accompanying the collision further act to fluidize a small body (Asphaug and Melosh, 1993). All in all, it appears that similar sized collisions larger than a few 100 km in scale, and perhaps as small as 10 km if actively heated internally, can be modeled using an inviscid approach. 3.2. Differentiation Fig. 11. Bodies of viscosity Z that are larger than rmin can deform to a strain e during a tidal collision. Smaller or more viscous bodies cannot accumulate the level of tidal viscous strain e on the timescale tgrav (Eq. (16)). The onset of significant prolate deformation is marked by e ¼ 1, while e ¼ 100 is catastrophically disruptive. The bulk density r ¼ 4 g cm3 is assumed in the calculation. Viscosity is non-Newtonian and is reduced by stress-dependent effects, pressure release, and by impact shocks in an actual collision; what is plotted is therefore an upper limit to rmin. The smallest impactor rmin that can come apart in an SSC in this viscous limit is found to be qffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi 2 ¼ Ze= 3pGr3 rmin ð16Þ by requiring the deformation rate e_ ¼ e=tgrav to be accommodated by the viscosity Z at a stress P0 . This expression (Asphaug et al., 2006) is plotted for various values of global strain e in Fig. 11, for terrestrial bodies of bulk density r 4 g cm3 . Strains of 1, 10, and 100 are plotted to bracket catastrophic disruption. Strain e \ 10 is allowed when viscosity is less than Z o Zmax 1013 ðr=1000 kmÞ2 ð17Þ where units are poise (g cm 1s 1). For comparison, mantle viscosity is thought to be 109 poise in convective models of early Earth (Walzer et al., 2004) and Z 109 21013 poise in Io asthenosphere models (Tackley, 2001). Partially molten Moonsized planets (Z C 1014 poise) can be approximated as fluid bodies, as can impactors as small as 10 km that are molten (Z 5108 poise). Because Zmax increases pr 2 , while Z decreases sensitively with size due to heat retention, the transition from viscous-limited to inviscid behavior is likely to be abrupt across some size threshold rmin. A number of effects make the response to similar-sized collisions fluid for bodies smaller than are plotted in Fig. 11. Rocks, partial melts and magmas are nonlinear fluids, whose effective linear viscosity decreases with a power of the stress. This means that viscosity Z s=e_ is much lower for larger-scale collisions because overburden stress P0 is larger by r2. Also, pressure release melting acts to lower the viscosity during tidal pressure unloading, of great significance to partially or nearly molten planets. The exolution of volatiles during pressure unloading can initially act to increase the viscosity of a magma by stiffening it with bubbles, but at high enough deformation and degassing rates the low viscosity of the gas wins out, and bulk viscosity plummets (see e.g. Gardner et al., 1999; Alidibirov and Dingwell, 1996). Interesting textures are expected. And lastly, any Viscosity’s exponential dependence on 1/T leads to a consideration for the heat sources available in planets before, during, and after a similar-sized collision, and to the behavior of differentiated (previously or presently melted) bodies versus undifferentiated bodies. During the primary phases of planetesimal formation, thermal energy is available from many sources, including impact shocks (from turbulence or infall), nebular shocks, solar heating, and the decay of short-lived radionuclides (see for instance Wasserburg and Papanastassiou, 1982). Burts of intense heating from an early sun would lead to some silicate melting in the innermost disk, but this heat source is not believed to be volumetrically important for terrestrial planet formation. Nebular heating by shocks can be intense, and shocks are proposed by Desch and Connolly (2002) to be responsible for the melting of silicate chondrules. The range of chondrule ages then requires that the solar nebula was present for several million years and that substantial gas and dust were present. Nebular shock heating would be prevalent and then diminish rapidly in pace with the accretion of planetesimals, due to the clearing out of the gas and dust which carries the shocks. As for impact shock heating, this is certainly a significant heat source during collisions in the late stage of giant impacts, but not during primary accretion when velocities are slow, following the initial stage of infall onto the disk. Compaction heating of porous cohesive aggregates during infall, or during the earliest growth within the disk, may be a relevant precursor to primary accretion. But hypervelocity collisions cannot contribute to the bulk melting of low-gravity bodies, simply because any melt products are shock-accelerated and escape. It is now generally acknowledged that the most important heat source for thermal processing during primary accretion was, in our solar system, the decay of 26Al - 26Mg, a radionuclide with half-life t1=2 ¼ 7:2 105 yr (Bizzarro et al., 2005). While the origin of 26Al is debated, its original abundance in our solar system is measurable in meteorites. For chondrites the initial 26Al/27Al C 5 106 , whose decay over t1=2 releases several times more heat (in erg g 1) than required to bring cold, dry dust to the melting point. Other short-lived radionuclides, notably 60Fe, were trapped in early-forming rocks in our solar system, also longspent but evidenced by their daughter products; their heat production is not believed to be as significant as 26Al in our own solar system. The prevalence of 26Al in other solar systems is unknown; this is a critical piece of missing knowledge since its presence or absence has the potential to dramatically alter the mechanism of primary accretion. A solar system with a small fraction of our measured 26Al might not produce enough heat for its early small bodies to melt. If small planetesimals remain unmelted, even as they grow larger than 100 km, then the character of their impact coagulation might change, conceivably even shifting the growth of planets away from the terrestrial planet-forming region, or biasing the favored sizes of finished planets. The rate of heat production dq=dt from radionuclide decay is proportional to the planet’s mass 43pr 3 r. Thermal energy dissipates by conducting through the solid and radiating from the planet’s surface area 4pr 2 at a temperature T, per unit area with a blackbody flux sT 4 . The heat produced, divided by heat Author's personal copy 212 E. Asphaug / Chemie der Erde 70 (2010) 199–219 radiated, thus increases with r, and increases greatly with temperature. Large planets thus attain radiative equilibrium at higher temperature and get hot enough to melt. According to 1D thermal modeling by Merk et al. (2002), a 10 km diameter homogeneous chondritic body melts if it accretes much faster than t1=2 (see Ghosh et al., 2006). Timing is everything, and so is location: planetesimals forming closer to the Sun acquire a greater fraction of Al-bearing silicates than those forming where ices dominate; they also accrete much more rapidly. They are thus much more prone to melting. The transition from fluid to solid behavior, plotted in Fig. 11 in terms of planetary radius, might be thought of as a transition in time from fluid to solid behavior, for the half-life of 26Al is—interestingly enough—comparable to the timescale of primary accretion. 3.3. Energy of collision Catastrophic disruption is defined as leaving a target body with no more than half of its original mass intact or gravitationally bound. In the target-centric view of things, the characteristic threshold of catastrophic disruption is traditionally expressed in terms of the specific impact kinetic energy 12 mv2imp per unit target mass M: 1 Q ¼ mv2imp =M 2 ð18Þ The disruption threshold Q* is the value of Q at which the final largest remnant M1 =M/2. For SSCs where m M the specific energy of impact must be defined as Q ¼ 12 mv2imp =ðM þ mÞ. One might then by analogy want to define Q* as forming a largest remnant with half the combined mass, M1 ¼ ðM þmÞ=2. This is inadequate for SSCs, since two just-grazing, equal-mass planets would each have half the total mass for any impact velocity. We must think of disruption in terms of the fates of both bodies. The impact kinetic energy per unit mass Q v2imp v2esc GM=R R2 is partitioned between the impactor and the target. The smaller of the colliding pair always suffers the greatest harm, and this is what makes hit-and-run collisions so transformative for the next-largest bodies in an accreting terrestrial planetary system. The tidal stress on the smaller by the larger, compared with the tidal stress on the larger by the smaller, is of greater magnitude in the smaller body in inverse proportion to its mass. In the case of direct collisions, the contact stress wave or shock wave is generated symmetrically about the contact front of a colliding pair, so that energy is partitioned equally into both bodies; energy density is also inversely proportion to mass. As for the impact differential stress, this can be thought of as the differential deceleration across the diameter of each colliding body, for instance in an off-axis SSC where half of the colliding mass is abruptly decelerated and half is not. If the contact forces are symmetric, then the smaller body decelerates more abruptly than the larger in inverse proportion to its mass. And so, as a rule of thumb, when planets of sizes r t R collide, then the specific tidal, gravitational, shear and shock stresses felt by each body scale inversely to the mass ratio g ¼ m=M. In the case of the Moon-forming simulation of Fig. 6, the impactor, being an order of magnitude less massive than the target, suffered an order of magnitude more damage, expressed as the gravitational, mechanical and shock energy of collision per unit mass. Whether shocks, tides or shears dominate an impactor’s disruption is a function of geometry, from just-grazing (where tides dominate) to head-on (where impact stresses and shocks dominate), and of scale. In an isolated planetesimal swarm with no bodies larger than 1000 km, random speeds are generally subsonic. But once Moon-sized planets exist, stirring the swarm to km/s velocities, the shock effects of impacts can become significant. 3.4. Enthalpy of unloading The gravitational binding energy of a uniform planet of mass M and radius R 3 UB ¼ GM 2 =R 5 ð19Þ is the energy required to disassemble a planet gently to infinity, and thus represents the lower limit of the kinetic energy 12 v2esc dm of all masses dm that contributed to the formation of the planet from v1 ¼ 0, with vesc increasing as the planet grows. The total kinetic energy of impacts is several times the binding energy for typically stirred up populations, going as 1 þ 1=2Y. This energy dissipates as heat, through shock and friction. For a planet the size of Mars, the gravitational binding energy is 8 1010 erg g1 . Assuming Safronov number Y 1 and dividing by the heat capacity of rock (cp 8 106 erg g1 K1 ) gives an estimate for the temperature increase due to impacts, of order 20,000 K (in which case constant heat capacity is not the right assumption). For a Vesta-sized planet, the same calculation gives an impact heating of only 100 K. Accretional heading of smaller asteroids is insignificant. A Mars-sized planet never gets this hot; it radiates to space. But some of the accretional energy is stored as internal energy u, and some is stored as enthalpy of compression, solution, and phase change. The specific enthalpy of a planetary interior is h ¼ u þP=r ð20Þ where P=r is the pressure times the specific volume V ¼ 1=r. Changes in enthalpy drive reactions: dh ¼ du þP dV þ V dP ð21Þ It is useful to think of SSCs in terms of enthalpy for the same reasons that enthalpy is the guiding state variable for the modeling of rising magmatic conduits (e.g. Wilson and Keil, 1991; Gardner et al., 1999). During large-scale similar sized collisions, the drop in pressure V dP as the planet comes apart leads to an abrupt change dh over the timescale tgrav , and this can drive various reactions forward. Hydrostatic pressure P increases with more than the square of a planet’s radius, since rocks are compressible. Holding the timescale of collisions tcoll tgrav as invariant in SSCs, both the pressure release DP and the rate of pressure release dP/dt scale greater than R2. The high magnitude and rate of unloading during disruption can drive cavitation, the dissolution of volatiles, bubble nucleation and coalescence, magmatic forcing, and pressure release melting. This causes us to look at the volcanic eruption modeling of Gardner et al. (1999) and others. Pressure unloading and its timescale for Vesta- to Mars-sized SSCs is comparable to strombolian-type eruptions, which are driven by gas bubbles rising faster than the surrounding melt. Measurements at Stromboli volcano in Italy (Burton et al., 2009) show gas slugs originating at 3 km depth. These same pressures are attained in the middle of a 500 km diameter planetary embryo. One might reason that strombolian eruption physics might be directly relevant to the degassing of large molten planetesimals in the aftermath of hit-and-run collisions, and their magmatic fragmentation (Alidibirov and Dingwell, 1996). As pressure is released, uncompensated pressure gradients result in accelerations that can change the dynamics of disruption, possibly contributing to the shedding of material or the emplacement of a debris disk. Pressure gradients played a role in the formation of the protolunar disk (Stevenson, 1987), and the disk formed not only from material released from impact shock pressure, but also from material that released from a high Author's personal copy E. Asphaug / Chemie der Erde 70 (2010) 199–219 pre-impact hydrostatic state P0. Most of the disk-forming material in the Moon-forming simulations (e.g. Fig. 6) emerges in the course of a few hours from several tens of kilobars of pressure, so even apart from the shock, the thermodynamic path is of critical importance. 3.4.1. Tidal collisions The best way to appreciate the physics of unloading is to isolate it in a purely tidal collision b \r þ R, so that the smaller planet does not hit the larger, but still comes deep inside the Roche limit Rroche ¼ 2:423RðrR =rr Þ1=3 ð22Þ Rroche is the threshold distance from a planet of radius R, density rR where an incompressible small fluid spheroid r, rr on circular orbit will be disrupted (Roche, 1850). The Roche limit is not strictly applicable to a parabolic or hyperbolic encounter, for which tidal disruption requires a somewhat closer periapse (Sridhar and Tremaine, 1992). For small strengthless incompressible bodies encountering massive planets at v1 ¼ 0, Asphaug and Benz (1996) found that periapse inside 0:69Rroche is the threshold for the shedding of matter, in agreement with the analytical result of Sridhar and Tremaine (1992); they found that passage inside of 0:55Rroche along a parabolic (v1 ¼ 0) trajectory results in the stripping of half the mass from the outer layers. The analysis breaks down for similar-sized tidal collisions because r R. The impactor is extensive, and part of it is on collision course when b r þ R. But ignoring this, if rR ¼ rr then 0:55Rroche C 1:3R, so that to first order we expect catastrophic tidal disruption when a planet r t 0:3R is on grazing parabolic incidence. Fig. 12 summarizes purely tidal encounters from the context of small spherical bodies of density 0.6 g cm 3 (‘‘comets’’) and 3 g cm 3 (‘‘asteroids’’) encountering planets of various density. It is seen that in the limit of r 5R, a catastrophically 213 disruptive tidal collision is about half as likely between an asteroid and Earth, as a physical collision. For comets tidal disruption is 50% more likely than a collision. For equal density bodies on parabolic encounters with r 5 R, tidal catastrophic disruption (M2 = m/2) is 13 as likely as collision. For studying compressible, differentiated planets undergoing tidal collisions, a self-gravitating hydrocode such as SPH remains the appropriate tool. Fig. 13 shows the result of a simulation (Asphaug et al., 2006) in which a Moon-size (0:01M ) differentiated terrestrial impactor, with composition 70 wt% rocky mantle and 30 wt% iron core as in the previous simulations, and the same Tillotson equation of state, encounters a Mars-size (0:1M ) impactor. The impactor is initially a non-rotating, isostatically equilibrated sphere. There is no physical contact, only gravitation and pressure unloading, so the target planet has been represented in the simulation as a point mass. The closest-approach velocity is 1:05vesc and the closest approach distance is b= 1.05(R+ r), and the bodies are of equal density. The two planets are represented in the center of mass frame, so that the larger (not shown) is displaced towards the top of the figure in each time step, while the smaller swings from the right towards the bottom and is severely deformed and stripped. The result of this slightly hyperbolic gravitational encounter is mass loss, spin-up, and global pressure unloading. The pressure drop is plotted in Fig. 14, which shows pressure inside the impactor normalized to the initial central pressure Pc ¼ 23 pGr2r r 2 , measured at the center of the planet (black) and at the core– mantle boundary (grey). Pressure unloading begins about half an hour before periapse, as the larger planet’s tidal field competes with the smaller’s self-gravity, and reaches a maximum of DP=P0 40250% about half an hour after the event. The unloading at the center takes slightly longer to complete, as the signal from surface mass removal propagates inward, and goes on for an hour after periapse. Permanent unloading by 20% results Fig. 12. Tidal disruption of small incompressible spheres of density rc ¼ 0:6 g cm3 (‘‘comets’’, left) and ra ¼ 3 g cm3 (‘‘asteroids’’, right) during parabolic (v1 ¼ 0) encounters with planets in our solar system: r ¼ 5:52 g cm3 (Earth), 1.66 (Neptune), 1.31 (Jupiter), 1.19 (Uranus), and 0.69 (Saturn), fitted to suites of simulations (Asphaug and Benz, 1996). The probability of a tidal event with a given level of disruption (M2 =m between 0 and 1, in the previous discussion), is plotted normalized to the probability of a physical collision. For example, the disruption of comet Shoemaker-Levy 9 was supercatastrophic (M2 =m 0:2) with periapse 1.31R. A tidal encounter this close or closer, but not impacting, is 0.2 times as likely as impact with Jupiter. Asteroids are catastrophically disrupted (M2 =m ¼ 0:5) by tides near terrestrial planets 12 as often as they collide; comets are catastrophically disrupted by tides near terrestrial planets 32 as often as they collide. Author's personal copy 214 E. Asphaug / Chemie der Erde 70 (2010) 199–219 Fig. 13. Tidal collision with closest approach velocity vimp ¼ 1:05vesc and closest approach distance b ¼ 1:05ðRþ rÞ, just beyond grazing; see Fig. 14. The impactor is Moonsize (0:01M ). The target is Mars-size (0:1M ), represented as an undeformable sphere which accretes any intersecting impactor particles. The simulation begins with a hydrostatic, non-rotating impactor at 5Rroche from the target, coming from the upper right. The snapshots are one per hour for 5 h around the periapse. The left plot shows the material (blue= rock, red =iron) in a slice through the symmetry plane. To the right are the corresponding pressures, in log code units, where orange 1011 dyn cm2 and blue t107 dyn cm2 . Tidal stresses and the shedding of matter and rotational stresses result in greatly reduced pressure, and greatly increased pressure gradients, making enthalpy available for melting and degassing in the disrupted arms of material. Fig. 14. Pressure unloading corresponding to the encounter in Fig. 13. Vertical axis is the pressure, divided by the central pressure of the planet. Pressures are averaged over particles near the planet’s center (black) and over the core–mantle boundary region (grey). Time is measured in hours before and after periapse. Global pressure unloading DP=P0 40250% begins about 12 h before periapse, due to tides, and continues for more than an hour after. Global pressure rises back to a base level that is 20% lower in the aftermath, due to spin-up and mass loss. From Asphaug et al. (2006). largest remnants is 90%, although the prelude to this pressure drop is a devastating shock-inducing collision. The encounter resembles two core bodies interacting gravitationally in a tidal collision, with mantle coming along for the ride; however the physics once fully explored is unlikely to be that simple. Fluid instabilities along the accelerating density boundary between the core and mantle may turn out to be as important as self-gravitational instability, in disrupting impactor cores; clues to the process are sought in the petrology of iron–silicate meteorites. The fate of undifferentiated bodies in response to disruptive tidal collisions is also complex. Shear localization is expected to generate frictional heating in a gravitational collision such as Fig. 13. The larger the planet the more energetic this frictional heating, producing melting (pseudotachylites) along shear planes. Planetesimals that are partially molten could melt entirely, or locally, as they cross the phase boundary during unloading from hydrostatic pressure; this could trigger core differentiation and initiate degassing. 4. Discussion from spin-up (the final body is rotating with a period 6 h) and mass loss. Faster hyperbolic tidal collisions involve unloading of shorter duration. In a hit-and-run collision with b or þ R, pressure unloading is greater, as the periapse is closer, but shock and collisional shearing play an increasing significant role as the fraction of intersected mass f increases. For disruptive hit-and-run collisions such as Fig. 7 d–f, the pressure unloading in the disrupted fragments is nearly 100%, because the material is now found in bodies with much smaller radii than before. In the case of Fig. 7d–f, the pressure drop experienced by material in the Earth finished accretion by mopping up dozens of Ceres- to Mars-sized bodies, becoming an amalgam of numerous smaller feeding zones (e.g. Chambers and Wetherill, 1998). One of these giant impacts formed the Moon, which is the archetypal unaccreted body. That is to say, the Moon is the unaccreted (though gravitationally bound) remnant of a highly selective process we call, as a whole, pairwise accretion, but which in fact is an ensemble of processes that can be seen in Fig. 8 to fall into four broad categories: (1) efficient accretion, (2) partial accretion, (3) erosion and disruption, and (4) hit-and-run. Author's personal copy E. Asphaug / Chemie der Erde 70 (2010) 199–219 Each has a unique outcome. Efficient accretion buries the evidence, resulting in isotopic and compositional homogeneity if the colliding planets are molten, or become molten as an outcome of the collision. It can also evidently lead to the formation of massive debris disks and major satellites like the Moon. Efficient accretion at the smallest scales might preserve the impacting bodies, for instance the layered-pile model for comets proposed by Belton et al. (2007). Partial accretion accretes higher density materials and loses lower-density materials, so that a planet that grows in this manner grows denser (iron rich and silicate and volatile poor) over time. Erosion is a continuum of the partial accretion curve in Fig. 8, in that a very inefficient partial accretion event is identical in process to an erosional collision, preferentially removing the outer materials which receive the brunt of the blow, and merging the inner materials; one is a net gain and the other a net loss. Disruption is in continuum with erosion. Catastrophic disruption requires impact energies far to the right of the plotted simulations. Except, that is, when one focuses on impactors that are disrupted by the targets that they strike, vice-versa. These hit-and-run planetary collisions are relatively newly explored planetary phenomena (Agnor and Asphaug, 2004a; Asphaug et al., 2006; Yang et al., 2007; Asphaug, 2009) and the degree to which they are relevant depends on the level of excitation of the accretionary system. In the regime where random velocities are several times faster than escape velocity, hit-and-run can largely be ignored since disruption and erosion are more likely to dominate (the case in the present asteroid belt, for instance) and cannot lead to the growth of planets. In the regime where random velocities are close to zero, hit-and-run is an exotic occurrence and perfect merger is the norm. But for velocity regimes inbetween, they are prevalent, so I conclude by venturing some specific contexts for hit-and-run. 4.1. Embedded embryos Wetherill (1994), in a series of groundbreaking papers establishing late stage planetary collisions, conducted Monte Carlo integrations of planet accumulation and found among other things that planets the size of the Moon and Mars may well have roamed the Main Belt for a few tens of Ma, until being scattered by mutual gravitational interactions and by resonant interactions with the giant planets. This opened up a new way of thinking about terrestrial planet evolution, and the origin and evolution of asteroids and the context of meteorites. Chambers (2007) postulated on the basis of N-body integrations that a planet might have survived between Mars and the inner Main Belt for hundreds of millions of years, until it became destabilized by chaotic interactions, as a candidate dynamical mechanism for the late heavy bombardment (LHB), the greatly enhanced impact flux recorded in lunar samples dated 3:924:0 Ga before present (reviewed in Chapman et al., 2007) and which may have been solar-system-wide. A planet near the Main Belt, once destabilized, would stir up the asteroids and greatly enhance the flux of impactors striking the terrestrial bodies. Petit et al. (2001) studied the primordial excitation and clearing of the Main Belt and found that Moon- to Mars-sized bodies would persist there for at least the first 10 Ma or longer. O’Brien et al. (2007) conducted similar N-body integrations and found that embryos of roughly a lunar mass could remain among the asteroids for up to the time of the LHB, to be scattered away along with the majority of asteroids, thus contributing to the excitation and loss of asteroidal mass until the larger embryos themselves were lost. This is all to say that the asteroids we see today in the Main Belt, and the somewhat larger progenitors from which they derived, are widely believed to have evolved early on, perhaps 215 even for the first 600 Ma until the LHB, in the presence of Moon-sized or larger embryos. The dynamical environment was excited by these embedded embryos, and thus was likely to have involved moderate random velocities v1 vesc . For large asteroid progenitors encountering these embedded embryos, hit-and-run would have been prevalent according to Fig. 8. If the scenario of embedded embryos is correct, then guided by Fig. 9 we can conclude that the Main Belt should be replete with hit and run survivors. In the outer solar system, where chaos during giant planet migration may have scattered as many as 10 Earth-masses of icy bodies beyond Neptune, of which perhaps 0:1M remains today (Levison and Morbidelli, 2003), the scenario is characteristically similar—almost total mass depletion that would include the loss of an ancestral population of somewhat larger bodies. The density ratio of rock:ice is similar to that of iron:rock, and thus, in lieu of suites of simulations for self-gravitating planetary bodies of ice– rock composition, the regimes of similar-sized collisions for icy bodies might be comparable to those shown in Fig. 8. If so, then among the differentiated bodies of the outer solar system, a number are expected to be stripped by hit-and-run collisions in the manner just described for the Main Belt. The dwarf planets beyond Neptune appear to have highly varying density, ranging from ice-like to rock-like (most recently, Fraser and Brown, 2009), and the relative velocities are too slow to allow for cataclysmic mantle stripping (e.g. Fig. 1). This diversity of ice:rock ratio is consistent with the idea that they, like their cousins in the Main Belt, underwent a late stage of growth involving hit-and-run collisions. 4.2. Recycled planetoids Hit-and-run events can lead to the formation of chains of recycled planetoids, the largest of them a few times smaller than r, as depicted in Fig. 7 d–f. The remnants in this particular simulation include about a dozen major bodies which form when a differentiated Moon-sized body strikes a Mars-sized body, at 301 from normal, at a velocity vimp ¼ 2vesc . The results are scale invariant given the caveats above. If we close our eyes to the rocky mantles of the colliding planets and consider only the cores, then the appearance is that of a planetary tidal disruption event such as comet Shoemaker-Levy 9 and its post-perijove ‘‘string of pearls’’ (Asphaug and Benz, 1996)—a linear structure with rather equant size and spacing. The intensely varying gravitational stresses, acting over tgrav , appear to play a dominant role in pulling the projectile core into pieces. As the core is deformed, instabilities at the rapidly shearing core–mantle interface may also play a major role in establishing fragment size and spacing. Because 23 of the colliding mass is in mantle silicates, whereas the iron cores appear to have their own intense tidal interaction, the event is very complex gravitationally, mechanically (core blobs plowing through the mantle rock), and in terms of the intense shock evolution, as the mantles respond to the direct hit. A layer of mantle silicates ranging from a dominant fraction to a thin veneer remain gravitationally bound to the blobs of core material that emerge from the collision. These new small planets are recycled from selected volumes of their parent planet materials, and have iron and silicate components that would not make sense in the context of standard models of planet formation and evolution. The major fragments are significantly iron-enriched, and the smaller debris are mostly of surface or mantle composition. At these relatively low numerical resolutions (tens of thousands of particles) more nuanced aspects of the collisions are unresolved. Higher fidelity simulations made possible by parallel SPH codes running on commodity supercomputers shall give a far better understanding of the major compositions, thermal and shock histories, spin states, and other Author's personal copy 216 E. Asphaug / Chemie der Erde 70 (2010) 199–219 aspects of the recycled planetoids, and to the long term fate of the escaping material. It is a complex phenomenon involving impact physics, tidal physics, solar system dynamics, meteoritics, and for internally molten planets, volcanology—the task is not just improving model resolution but also the model physics. But for now, a few observations can be made: The final bodies in a chain-forming hit and run collision are composed of deep interior materials that find themselves, in the course of hours, at greatly reduced hydrostatic pressure P0. This creates a potential for volumetric degassing and the fluxing of water and other previously dissolved volatiles in response to intense, abrupt pressure disequilibrium. Shock intensity is highly variable, since they form from materials at a considerable distance from the collisional contact surface. So in general one expects a wide variety of metamorphic and igneous evolution to occur in this small stretch of time, leading to diverse pathways for meteorite petrogenesis. Regarding iron and iron–silicate meteorites, the surface area of iron to silicate is greatly increased during a chain-forming hit and run event, since the original impactor core is parceled into a dozen or so new planetoids, and is sheared against the silicate interface as it happens. When a core body is sheared into multiple components, shear localization is expected to occur along the core–mantle interface, causing detachment and intense friction. Thus, the prevalence of mesosiderites, pallasites, and other iron–silicate mechanical mixtures, and their diversity, is consistent with this type of parent body mechanical-driven evolution. Shear localization does not require a core–mantle interface; evidence for pseudotachylitic clasts and textures in ordinary chondrite meteorites (van der Bogert et al., 2003) may indicate the mechanical shearing of undifferentiated planetary bodies as well, perhaps during smaller-scale early-epoch SSCs at lower velocity. Indeed while most of this review has focused on the implications of SSCs for differentiated bodies, for which the before-and-after change is the most spectacular, the process applied to undifferentiated bodies can lead to various kinds of evolution ranging from hydrothermal action, to pseudotachylitic modification, to brecciation. Direct evidence for a chain-forming hit-and-run collision is perhaps recorded in the IVA iron meteorites, one of the 14 major meteorite groups. Each iron meteorite group corresponds to an original reservoir (planetesimal core) that is a unique alloy of iron and nickel, plus trace metals such as gold. Thus the 14 major iron meteorite groups represent 14 parent bodies, while there are hundreds of unclassified iron meteorites, bringing the total number of disrupted parent bodies represented by iron meteorites up to 50–100. One immediately must ask: How is it that so many large differentiated asteroids underwent catastrophic breakup—especially when other asteorids, especially 4 Vesta (Davis et al., 1985), did not? According to Ni–Fe measurements by Rasmussen et al. (1995), the IVA irons have metallographic cooling rates spanning almost 2 orders of magnitude, from 19–3400 K/Ma. Yang et al. (2007) report revised cooling rates for this group spanning 100–6000 K/Ma, and show a trend of faster cooling rate for lower bulk Ni. To satisfy the most rapid of these cooling rates, and to conform to the bulk Ni data, Yang et al. develop a model where the IVA meteorites cooled within a 300 km diameter metallic body that was stripped bare of its mantle. Mantle removal is required by the most rapid cooling rates, simply because an insulating mantle would cause the iron core to cool slowly, and under nearly isothermal conditions. The wide span in cooling rates within a single stripped core body remains problematic in this scenario, but it is consistent with the cosmic ray exposure ages that indicate cooling within a single final body. Stripping a Vesta-sized mantle bare is also possible in a chainforming hit-and-run collision; also recall that repeat hit-and-runs may have occurred (Fig. 9). Diverse cooling rates are an expected result when a core is pulled into a chain of new planets, each with its own core, its own mantle (or lack thereof), its own diameter and cooling rate. The scenario of Fig. 7 d–f would lead to the formation of a handful of new bodies each with the same major elemental and initial isotopic core composition; each would subsequently follow its own evolution as a minor planet. Iron meteorites derived from these bodies would come from the same parent body, compositionally, but from different bodies in terms of their solidification, cooling, and post-formation physical and chemical history, and cosmic-ray exposure ages of their resultant meteorites. As for the silicate portions of these strung-out new planets, there would be much greater variation in composition owing to the initial shock state, varying provenance within the initial projectile’s mantle, mixing with the target mantle, and volatile dissolution. As for that broad and most controversial topic of early solar system origins, the formation of chondrules, it is certainly not farfetched to consider that hot, possibly molten bodies tens to hundreds of km diameter would have undergone collisional evolution at random speeds comparable to their vesc, in the first few Ma when 26Al was active. If so, then a similar-sized collision scenario for chondrule formation is worth considering, in which molten asteroids are torn apart once or twice for every efficient accretion, as part of the inefficient process of accretion during random stirring. If hit and run collisions happen to a given parcel of matter many times over as Fig. 9 suggests, and if those parcels are molten and gas-rich, then pressure unloading would result in the dispersal of material over tgrav hours, under phreatic conditions. It can be thought of as an evolution of the chondrule formation hypothesis of Sanders and Taylor (2005), but with pressure unloading and the associated droplet formation physics and timescale taking the place of impact splashing. It is dynamically and chemically plausible, and recommends further research into the earliest thermophysical processing of terrestrial planet-forming materials during similar-sized collisions. 4.3. Mercury and Mars Mercury is anomalously iron-rich, about 70% by mass. Benz et al. (1988, 2007) showed that a giant impact with random velocity 6vesc by an projectile r R=2 (depending on impact angle) is capable of shock-accelerating half of Mercury’s mantle to escape velocity, in an intensely energetic collision bearing over 30 times the specific energy of the giant impact proposed to have formed the Moon. One of the challenges to the hypothesis is compositional, for there is geophysical and spectroscopic evidence (for instance Kerber et al., 2009; Sprague et al., 1995) for volatiles in the crust of Mercury in much greater abundance than on the Moon. This could be challenging to reconcile with the hypothesis of the planet finishing its evolution by having its mantle shocked and dispersed into space, and part-reaccumulated. Benz et al. (2007) show that the ejected material, which goes to occupy a torus around the Sun centered on Mercury’s orbit, is fragmented into sizes small enough for most to be removed by Poynting–Robertson drag; the rest reaccretes to form the new upper mantle. However, Gladman and Coffey (2009) find that the opacity of this debris cloud will severely limit the rate of mass removal (and incidentally, will put the other planets into total shadow). We knew from the start (Fig. 1) that it is not easy to blast off a planetary mantle. If the event requires a collision that is anomalously fast and energetic, it seems odd that the lowest possible impact velocity (parabolic encounter) is invoked to Author's personal copy E. Asphaug / Chemie der Erde 70 (2010) 199–219 217 5. Conclusions 1 0.8 60 M2/m 0.6 45 0.4 0.2 30 0 0.5 1 1.5 2 v-innity / v-escape 2.5 3 Fig. 15. Mass of the largest impactor remnant (M2 r m) after a hit-and-run collision, for the g ¼ 0:1 (m ¼ 0:1M) subset of the collisions in Fig. 8. Calculations by Agnor and Asphaug (2004b). The curves are for different impact angles, labeled. The missing points to the left of the graphs for 301 and 451 are events where the impactor and target accrete, so that there is no sizable M2; the transition from accretion to hit-and-run is abrupt with changes in y and v1 . To the lower right of the 301 graph the transition is gradual towards M2 -0; here the impactor is unaccreted but the escaping matter is disrupted with increasing energy into smaller sizes. Inbetween are outcomes that leave behind a substantial portion (or portions) of impactor mass m. The chain-forming collision of Fig. 7d–f plots here with a largest fragment mass M2 =0.2m; the outcome is actually several new bodies of which the largest is plotted. For the most typical impact angle of 451, for moderately excited random velocities, the impactor loses between 13 and 23 its mass in a hit-and-run, a conjecture to be studied further for the origin of Mercury. explain the Moon’s formation, whereas an anomalously hyperbolic impact (vimp b vesc ) is invoked to explain Mercury, both during the same late stage of solar system history. By directly scaling from Figs. 8 and 9, an alternative giant impact scenario is proposed that would remove Mercury’s mantle at a characteristic impact velocity v1 vesc , assuming Mercury was the impactor rather than the target. What did it run into? Wetherill (1992) showed that Mercury could have originated beyond Mars, leading to the possibility that it may have encountered proto-Earth or proto-Venus. Perhaps more dynamically probable is for Mercury, under quieter circumstances, to have become sufficiently eccentric to encounter Venus or protoVenus in the course of later chaos (perhaps swapping its volatiles over time onto the larger planet as described earlier). The basic hypothesis is that Mercury started out rather Marslike and collided with a larger planetary embryo along the way, emerging from the hit-and-run as a planet of roughly Mercury’s mass and composition, in a process akin to Fig. 7a–c. In this simulation the final impactor lost 35% of its original mass (M2 = 0.65 m) which equals half its mantle. Largest remnant masses (normalized to impactor mass) for the simulations plotted in Fig. 8 were computed by Agnor and Asphaug (2004a, b) for the simulations described above and are plotted in Fig. 15. Mercury may thus have formed more closely akin to how the Moon formed: a Mars-mass planet running into a larger planet, but in Mercury’s case a fraction faster. Still, we must keep in mind that Mercury’s bulk composition may not be defined by any single giant impact. For instance, if somewhat higher random velocities v1 =vesc existed near Mercury throughout the late stage, this might account for a systematic increase in disruptive and hit-and-run collisions (e.g. the black diamonds in Fig. 9) leading to a hierarchical evolution towards iron-rich composition. Numerical simulations have shown that impacting bodies of similar size can experience hit and run collisions for the random velocities typical of late stage planet formation. This causes us to consider giant impacts from the surviving impactor’s perspective. Hit-and-run is an efficient mechanism for dismantling the smaller of a colliding pair, removing its outer layers and causing global transformations, while leaving the target body comparatively intact. If Main Belt bodies Moon-sized or larger once existed, as is expected on the basis of dynamical studies, then Main Belt asteroids ought to be replete with hit and run collisional relics. Vesta, whose crust appears to be largely intact, may have been lucky to avoid a major hit-and-run, but suffered a typical bombardment by smaller impactors. This scenario requires only a moderate anomaly for Vesta, compared to the alternative, that Psyche, Kleopatra, and the parent bodies of the dozens of families of iron meteorites were beaten down to their cores by erosive and disruptive impacts, with Vesta somehow dodging a cosmic fusillade. If Vesta avoided a hit and run collision until the larger bodies left the Main Belt, while Psyche was dismantled to its core, perhaps hit-and-run evolution happens to about half the NLBs in late solar system history. For the small terrestrial planets, we might in this context look at Mars as a body which has always been among the very largest of its collisional population, efficiently sweeping up smaller planetesimals and embryos and being little bothered by hit and run collisions. We might then look at Mercury as a typical next-largest body, a hit-and-run remnant having lost its mantle. Meteorites show evidence for hit and run collisions. A hit-andrun collision can account for the wide range in cooling rates exhibited within one or two families of iron meteorites (Yang et al., 2007). Chondrite meteorites show the kinds of frictional or even pseudotachylitic textures that are expected during similar sized collisions, although hit-and-run is difficult to discern among undifferentiated planets where there is no core–mantle segregation. These frictional and breccia textures, and evidence for altered and metamorphosed silicate bodies (Keil, 2000), and the overall stunning variety and relative abundance of iron and iron– silicate meteorites, are not direct evidence for hit and run collisions per se, but are certainly indicative that similar sized collisional processes have been at work, along with the associated processes described above. Chondrites, the most abundant meteorites, derive from the most common parent bodies in the Main Belt. They have not been subjected to temperatures close to melting since the time of chondrule formation, a few million years after solar system formation. Chondrules, which might account for over half the mass of the Main Belt (Scott, 2007), are solidified silicate droplets from an epoch of transient heating episodes. In the first 105–106 yr of planetesimal growth, if molten 10–100 km diameter precursor bodies were kept heated by 26Al decay, but undifferentiated because of their very low gravity, then it is conceivable that the abrupt (strombolian) pressure unloading experienced by molten but undifferentiated small precursor bodies could result in ubiquitous small melt droplets among the remnants that did not accrete. Chondrules forming by such a mechanism would either disperse into space, and either be removed or reaccreted, or collapse en masse gravitationally on a timescale tgrav , which for a dense plume of droplets would be a few hours. If a planet grows to become one of the largest, then there is nothing larger to collide into and it becomes an amalgam of its feeding zone (Chambers and Wetherill, 1998). Impacts by smaller bodies batter their outer layers for the remainder of their evolution, and can remove atmospheres and oceans (Genda and Abe, 2005) and even hemispheres of crust (Nimmo et al., 2008; Author's personal copy 218 E. Asphaug / Chemie der Erde 70 (2010) 199–219 Marinova et al., 2008), but the removal of their mantles requires collisions of unusually high energy. The cores of accreted planets are not disrupted for expected impact velocities (Scott et al., 2001). A very massive and wayward impactor is required to remove the fraction of Mercury’s mantle that appears to be missing, assuming it began with Earth-like bulk composition (Benz et al., 2007). This scenario is dynamically opposite the Moon-forming scenario, for which the impactor and target must be almost identical dynamically and chemically, falling in at v1 0. But in Moon-forming giant impact scenarios, models (Canup and Asphaug, 2001) show that the Mars-sized impactor would escape if going a fraction faster. This motivates an alternative scenario in which Mercury sheds its mantle in a hit and run collision with a larger protoplanet early on, at v1 vesc (e.g. Fig. 7a–c) or conceivably during later chaos encountering Venus. Hit and run collisions occur in extrasolar planet-forming systems. Exoplanets are being discovered through transit observations to include ‘‘super-Earths’’ that are several times more massive than our own (e.g. Ribas et al., 2008); the discovery of the first Earth-mass planet is imminent. But how Earth-like can a planet be, in a solar system that has accreted one or more superEarths? Where Earths are the unaccreted NLBs, most will have lost their crusts, oceans and atmospheres at one time or another, or been dismantled like Mercury, on the perilous path of planetary growth. It may be that in order to have water-bearing Earth-mass terrestrial planets, they need to accrete as the largest bodies in the population. Acknowledgments This research was sponsored by NASA’s Planetary Geology and Geophysics Program (‘‘Small Bodies and Planetary Collisions’’) and Origins of Solar Systems Program (‘‘Meteorite and Dynamical Constraints on Planetary Accretion’’) under Research Opportunities in Space and Earth Sciences. The SPH computations were performed on the NSF-funded supercomputer upsand at UCSCIGPP. My research into planet-scale collisions began as a thesis project with Willy Benz, whose subsequent collaboration on tidal disruption led me to try understanding hit and run collisions. This research evolved through collaborations with Robin Canup on Moon formation, and with Craig Agnor, a patient explainer of planetary dynamics. I am grateful to John Chambers and Bill Bottke for their careful reviews and unique insights. I thank Ed Scott, Quentin Williams, Francis Nimmo, Jeff Cuzzi and Naor Movshovitz for creative critical discussions, and Klaus Keil for his original thinking on igneous and evolved asteroids and for inviting me to write this review. References Agnor, C., Asphaug, E., 2004a. The Astrophysical 613, L157. Agnor, C., Asphaug, E., 2004b. In: AGU Fall Meeting Abstracts, p. A2+ . Agnor, C.B., Canup, R.M., Levison, H.F., 1999. Icarus 142, 219. Alidibirov, M., Dingwell, D.B., 1996. Nature 380, 146. Asphaug, E., 1997. Meteoritics and Planetary Science 32, 965. Asphaug, E., 2009. Annual Review of Earth and Planetary Sciences 37, 413. Asphaug, E., Agnor, C., 2005. In: Bulletin of the American Astronomical Society. Bulletin of the American Astronomical Society, vol. 37, pp. 623–+ . Asphaug, E., Agnor, C.B., Williams, Q., 2006. Nature 439, 155. Asphaug, E., Benz, W., 1994. Nature 370, 120. Asphaug, E., Benz, W., 1996. Icarus 121, 225. Asphaug, E., Melosh, H.J., 1993. Icarus 101, 144. Belton, M.J.S., Thomas, P., Veverka, J., Schultz, P., A’Hearn, M.F., Feaga, L., Farnham, T., Groussin, O., Li, J., Lisse, C., McFadden, L., Sunshine, J., et al., 2007. Icarus 187, 332. Benz, W., Anic, A., Horner, J., Whitby, J.A., 2007. Space Science Reviews 132, 189. Benz, W., Asphaug, E., 1999. Icarus 142, 5. Benz, W., Cameron, A.G.W., Melosh, H.J., 1989. Icarus 81, 113. Benz, W., Slattery, W.L., Cameron, A.G.W., 1988. Icarus 74, 516. Bizzarro, M., Baker, J.A., Haack, H., Lundgaard, K.L., 2005. The Astrophysical Journal 632, L41. Bottke, W.F., Durda, D.D., Nesvorný, D., Jedicke, R., Morbidelli, A., Vokrouhlický, D., Levison, H., 2005. Icarus 175, 111. Burbine, T.H., Meibom, A., Binzel, R.P., 1996. Meteoritics and Planetary Science 31, 607. Burton, M.R., Caltabiano, T., Mure , F., Salerno, G., Randazzo, D., 2009. Journal of Volcanology and Geothermal Research 182, 214. Cameron, A.G.W., Benz, W., 1991. Icarus 92, 204. Canup, R.M., 2004. Annual Review of Astronomy and Astrophysics 42, 441. Canup, R.M., 2008. Icarus 196, 518. Canup, R.M., Asphaug, E., 2001. Nature 412, 708. Chambers, J.E., 2007. Icarus 189, 386. Chambers, J.E., Wetherill, G.W., 1998. Icarus 136, 304. Chambers, J.E., Wetherill, G.W., 2001. Meteoritics and Planetary Science 36, 381. Chandrasekhar, S., 1969. Ellipsoidal Figures of Equilibrium. Yale University Press, New Haven. Chapman, C.R., Cohen, B.A., Grinspoon, D.H., 2007. Icarus 189, 233. Cuzzi, J.N., Hogan, R.C., Paque, J.M., Dobrovolskis, A.R., 2001. Astrophysical Journal Letters 546, 496. Cuzzi, J.N., Hogan, R.C., Shariff, K., 2008. Astrophysical Journal 687, 1432. Davis, D.R., Chapman, C.R., Weidenschilling, S.J., Greenberg, R., 1985. Icarus 62, 30. Desch, S.J., Connolly Jr., H.C., 2002. Meteoritics and Planetary Science 37, 183. Dixon, J.E., Stolper, E., Delaney, J.R., 1988. Earth and Planetary Science Letters 90, 87. Dohnanyi, J.W., 1969. Journal of Geophysical Research 74, 2531. Dominik, C., Blum, J., Cuzzi, J.N., Wurm, G., 2007. In: Reipurth, B., Jewitt, D., Keil, K. (Eds.), Protostars and Planets V, pp. 783–800. Fraser, W., Brown, M.E., 2009. AAS/Division for Planetary Sciences Meeting Abstracts, vol. 41, 65.03. Gardner, J.E., Hilton, M., Carroll, M.R., 1999. Earth and Planetary Science Letters 168, 201. Genda, H., Abe, Y., 2005. Nature 433, 842. Ghosh, A., Weidenschilling, S.J., McSween, H.Y., Jr., Rubin, A., 2006. In: Meteorites and the Early Solar System II, pp. 555–566. Gladman, B.J., Coffey, J., 2009. Meteoritics and Planetary Science 44, 285. Gomes, R., Levison, H.F., Tsiganis, K., Morbidelli, A., 2005. Nature 435, 466. Grady, D.E., Kipp, M.E., 1985. Journal of Applied Physics 58, 1210. Greenberg, R., Hartmann, W.K., Chapman, C.R., Wacker, J.F., 1978. Icarus 35, 1. Hahn, J.M., Rettig, T.W., 2000. Icarus 146, 501. Hartmann, W.K., Davis, D.R., 1975. Icarus 24, 504. Holsapple, K., Giblin, I., Housen, K., Nakamura, A., Ryan, E., 2002. Asteroids III, 443. Holsapple, K.A., 1993. Annual Review of Earth and Planetary Sciences 21, 333. Jeffreys, H., 1947. Monthly Notices of the Royal Astronomical Society 107, 260. Johansen, A., Oishi, J.S., Low, M.-M.M., Klahr, H., Henning, T., Youdin, A., 2007. Nature 448, 1022. Jutzi, M., Benz, W., Michel, P., 2008. Icarus 198, 242. Jutzi, M., Michel, P., Hiraoka, K., Nakamura, A.M., Benz, W., 2009. Icarus 201, 802. Kamenetsky, V.S., Kamenetsky, M.B., Sharygin, V.V., Golovin, A.V., 2007. Geophysical Research Letters 34, 9316. Kaula, W.M., 1990. In: Newsom, H.E., Jones, J.H. (Eds.), Origin of the Earth, 45. Keil, K., 2000. Planetary and Space Science 48, 887. Keil, K., Haack, H., Scott, E.R.D., 1994. Planetary and Space Science 42, 1109. Kelley, S.P., Wartho, J.-A., 2000. Science 289, 609. Kerber, L., Head, J.W., Solomon, S.C., Murchie, S.L., Blewett, D.T., Wilson, L., 2009. Earth and Planetary Science Letters 285, 263. Kokubo, E., Ida, S., 1998. Icarus 131, 171. Korycansky, D.G., Asphaug, E., 2006. Icarus 181, 605. Levison, H.F., Morbidelli, A., 2003. Nature 426, 419. Marcus, R.A., Stewart, S.T., Sasselov, D., Hernquist, L., 2009. Astrophysical Journal Letters 700, L118. Marinova, M.M., Aharonson, O., Asphaug, E., 2008. Nature 453, 1216. Melosh, H.J., 1989. Impact Cratering: A Geologic Process. Melosh, H.J., Ryan, E.V., Asphaug, E., 1992. Journal of Geophysical Research 97, 14735. Merk, R., Breuer, D., Spohn, T., 2002. Icarus 159, 183. Meyer, M., Carpenter, J., Mamajek, E., Hillenbrand, L., Hollenbach, D., Moro-Martin, A., Kim, J., Silverstone, M., Najita, J., Hines, D., Pascucci, I., Stauffer, J., et al., 2008. The Astrophysical Journal Letters 673, L181. Morbidelli, A., Bottke, W.F., Nesvorný, D., Levison, H.F., 2009. Icarus 204, 558. Morbidelli, A., Moons, M., 1993. Icarus 102, 316. Nimmo, F., Agnor, C.B., 2006. Earth and Planetary Science Letters 243, 26. Nimmo, F., Hart, S.D., Korycansky, D.G., Agnor, C.B., 2008. Nature 453, 1220. O’Brien, D.P., Morbidelli, A., Bottke, W.F., 2007. Icarus 191, 434. O’Brien, D.P., Morbidelli, A., Levison, H.F., 2006. Icarus 184, 39. Petit, J.-M., Morbidelli, A., Chambers, J., 2001. Icarus 153, 338. Pierazzo, E., Melosh, H.J., 2000. Annual Review of Earth and Planetary Sciences 28, 141. Porritt, L.A., Cas, R.A.F., 2009. Journal of Volcanology and Geothermal Research 179, 241. Rasmussen, K.L., Ulff-Møller, F., Haack, H., 1995. Geochimica et Cosmochimica Acta 59, 3049. Author's personal copy E. Asphaug / Chemie der Erde 70 (2010) 199–219 Ribas, I., Font-Ribera, A., Beaulieu, J.-P., 2008. Astrophysical Journal Letters 677, L59. Richardson, D.C., Bottke, W.F., Love, S.G., 1998. Icarus 134, 47. Roche, E., 1850. La figure d’une masse fluide soumise a l’attraction d’un point éloginé, Acad. des Sd. de Montepellier 1, 243. Safronov, V.S., 1972. Evolution of the Protoplanetary Cloud and Formation of the Earth and Planets. Safronov, V.S., Zvjagina, E.V., 1969. Icarus 10, 109. Sanders, I.S., Taylor, G.J., 2005. In: Chondrites and the Protoplanetary Disk, ASP Conference Series 341, 915. Schäfer, C., Speith, R., Kley, W., 2007. Astronomy and Astrophysics 470, 733. Schenk, P.M., Asphaug, E., McKinnon, W.B., Melosh, H.J., Weissman, P.R., 1996. Icarus 121, 249. Scott, E.R.D., 2007. Annual Review of Earth and Planetary Sciences 35, 577. Scott, E.R.D., Haack, H., Love, S.G., 2001. Meteoritics and Planetary Science 36, 869. Shoemaker, E.M., 1962. Interpretation of lunar craters. In: Physics and Astronomy of the Moon. Academic Press, New York, pp. 283–351. Sprague, A.L., Hunten, D.M., Lodders, K., 1995. Icarus 118, 211. Sridhar, S., Tremaine, S., 1992. Icarus 95, 86. Stevenson, D.J., 1987. Annual Review of Earth and Planetary Sciences 15, 271. Tackley, P.J., 2001. Journal of Geophysical Research 106, 32971. 219 van der Bogert, C.H., Schultz, P.H., Spray, J.G., 2003. Meteoritics and Planetary Science 38, 1521. Walzer, U., Hendel, R., Baumgardner, J., 2004. Tectonophysics 384, 55. Wasserburg, G.J., Papanastassiou, D.A., 1982. In: Essays in Nuclear Astrophysics, 77. Weibull, W., 1939. Ingeniörs Vetenskaps Akademien 151, 45. Weidenschilling, S.J., 2008. In: Proceedings of the Nobel Symposium 135, Physica Scripta T130 014021. Weissman, P.R., Asphaug, E., Lowry, S.C., 2004. Comets II, 337. Wetherill, G.W., 1976. Lunar and Planetary Science Conference Proceedings. Lunar and Planetary Science Conference Proceedings, vol. 7, pp. 3245–3257. Wetherill, G.W., 1980. Annual Review of Astronomy and Astrophysics 18, 77. Wetherill, G.W., 1985. Science 228, 877. Wetherill, G.W., 1992. Icarus 100, 307. Wetherill, G.W., 1994. Geochimica et Cosmochimica Acta 58, 4513. Wilson, L., Keil, K., 1991. Earth and Planetary Science Letters 104, 505. Wurm, G., Blum, J., 2006. Experiments on planetesimal formation. In: Planet Formation, 90. Yang, J., Goldstein, J.I., Scott, E.R.D., 2007. Nature 446, 888. Yin, Q., Jacobsen, S.B., Yamashita, K., Blichert-Toft, J., Télouk, P., Albare de, F., 2002. Nature 418, 949.
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