LIGO: PROGRESS AND PROSPECTS Barry C. Barish California Institute of Technology, Pasadena, CA 90405, USA ABSTRACT The status, progress and plans for the Laser Interferometer Gravitational-wave Observatory (LIGO) are presented. Ground based gravitational wave detectors are complementary to the initiatives in space. The ground-based detectors will cover higher frequencies (10 to 10 4 Hz) and will therefore be sensitive to different sources or different regimes for the same astrophysical source. INTRODUCTION The Laser Interferometer Gravitational-wave Observatory (LIGO) is a joint Caltech-MIT project supported by the National Science Foundation (Barish and Weiss, 1999). The LIGO observations will be carried out with long baseline suspended mass interferometers that are located at Hanford, Washington and Livingston, Louisiana. To unambiguously make detections of these rare events a time coincidence within 10ms (transit time at the speed of light) between detectors separated by 3030 km will be sought. The construction of LIGO has been completed and the two facilities can be seen in the aerial photograph in Figure 1. Fig 1. Aerial photographs of the 4km long suspended mass interferometers installed a Livingston, Louisiana on the left and Hanford, Washington on the right are shown. 2 LIGO is now entering the commissioning phase for this complex instrument. Following a planned two year commissioning program, we expect the first dedicated sensitive broadband searches for astrophysical gravitational waves at an amplitude (strain) of h ~ 10-21 to begin during 2002. The initial search with LIGO will be the first attempt to detect gravitational waves with a detector having sensitivity that intersects plausible estimates for known astrophysical source strengths. The initial detector constitutes a 100 to 1000 fold improvement in both sensitivity and bandwidth over previous searches. The facilities developed to support the initial interferometers will allow for the evolution of the detectors to probe the field of gravitational wave astrophysics with more and more sensitivity over the next two decades. Sensitivity improvements and special purpose detectors will be needed either to enable detection if strong enough sources are not found with the initial interferometer, or following detection, to increase the rate in order to enable the detections to begin to become a new tool for astrophysical research. The other detectors in the world offer potential simultaneous detection of astrophysical sources and there are plans underway to correlate signals from all operating detectors in a worldwide network. THE LIGO SUSPENDED MASS INTERFEROMETERS The optical configuration in LIGO is a power recycled Fabry-Perot Michelson interferometer. It is this type of configuration that will be used for the initial interferometers. The layout and parameters are shown in Figure 2. There are many other possible types of interferometer configurations that have been considered and might be used in future detectors. Considerable research has been done at Stanford on Sagnac interferometers, as the power of the lasers increase an all reflective geometry might be used, and there is considerable work toward adding a signal recycling mirror on the output side of the interferometer, allowing an ability to tune the interferometer for increased sensitivity at a particular frequency in a narrow band mode. The initial LIGO interferometer parameters have been chosen such that the sensitivity will be consistent both with estimates needed for possible detection of known sources. Although the rate for such sources have large uncertainty, improvements in sensitivity linearly improves the distance searched for detectable sources, which increases the rate by the cube of the improvement. Our plans are to upgrade the detector in about 2006 with improved mirrors, suspensions, seismic isolation and laser giving about a factor of 20 sensitivity improvement, and to also add the signal recycling feature for narrow band searches. Fig 2. The optical layout of the LIGO suspended mass Michelson interferometer with Fabry-Perot arm cavities Fig 3. The limiting and other noise sources for LIGO are shown. The shaded area indicates the detector sensitivity. 4 Noise Sources and Sensitivity The success of the detector ultimately will depend on how well we are able to control the noise in the measurement of very small strains. Noise is broadly but also usefully categorized in terms of those phenomena which limit the ability to sense and register the small motions (sensing noise limits) and those that perturb the masses by causing small motions (random force noise). Eventually one reaches a practical but not fundamental limiting noise, the quantum limit, which combines the sensing noise with a random force limit. This orderly and intellectually satisfying categorization presumes that one is careful enough as experimenters in the execution of the experiment that one has not produced less fundamental, albeit, real noise sources that are caused by faulty design or poor implementation. We have dubbed these as technical noise sources and in real life these have often been the impediments to progress. The primary noise sources for the initial LIGO detector are shown in Figure 3. In order to control the technical noise sources, extensive use has been made of two concepts. The first is the technique of modulating the signal to be detected at frequencies far above the 1/f noise due to the drift and gain instabilities experienced in all instruments. For example, the optical phase measurement to determine the motion of the fringe is carried out at radio frequency rather than near DC. Thereby, the low frequency amplitude noise in the laser light does not directly perturb the measurement of the fringe position. (The low frequency noise still causes radiation pressure fluctuations on the mirrors through the asymmetries in the interferometer arms.) A second concept is to apply feedback to physical variables in the experiment to control the large excursions at low frequencies and to provide damping. The variable is measured through the control signal required to hold it stationary. Here a good example is the position of the interferometer mirrors at low frequency. The interferometer fringe is maintained at a fixed phase by holding the mirrors at fixed positions at low frequencies. Feedback forces to the mirrors effectively hold the mirrors “rigidly”. In the initial LIGO interferometers the forces are provided by permanent magnet/coil combinations. The mirror motion that would have occurred is then read in the control signal required to hold the mirror. Great care has been taken in LIGO to control these technical noise sources. In order to test and understand our sensitivity and the noise limitations, we have performed extensive tests with a 40-meter prototype interferometer on the Caltech campus. This interferometer has essentially all the pieces and Fig 4. The displacement noise measured in the the same optical configuration as is used in LIGO, so LIGO 40m suspended mass interferometer prototype it represents a good place to demonstrate our on the Caltech campus. The general shape and level understanding of these issues before confronting are well simulated by our understanding of the them in LIGO. The 40m prototype has achieved a limiting noise sources: seismic noise at the lowest displacement sensitivity of h ~ 10-19 m, which is frequencies; suspension thermal noise at the comparable to the displacement sensitivity required intermediate frequencies; and shot noise or in the 4 km LIGO interferometers. Figure 4 shows photostatistics at the highest frequencies. Also, the the measured noise curve in the 40m prototype and primary line features are understood as various our understanding of the contributions from various resonances in the suspension system. noise sources. ASTROPHYSICAL SOURCES OF GRAVITATIONAL WAVES There are a many known astrophysical processes in the Universe that produce gravitational radiation (Thorne 1987). Terrestrial interferometers, like LIGO, will search for signals from in the 10Hz - 10KHz frequency band. Characteristic signals from astrophysical sources will be sought over background noise from continuously recorded time-frequency series of the strain. Examples of sources and their characteristic signals include the following: Chirp Signals The inspiral of compact objects such as a pair of neutron stars or black holes gives radiation that characteristically increases in both amplitude and frequency as the system evolves toward its the final coalescence. This characteristic ‘chirp signal’ can be calculated in detail, and the final waveform is sensitive to the masses, separation, ellipticity of the orbits, etc. A variety of search techniques have been developed, including a direct comparison with an array of templates that cover the range of possible parameters. The waveform for the inspiral phase is well understood and has been calculated in sufficient detail for neutron star-neutron star inspiral. This inspiral phase is well matched to the LIGO sensitivity band for neutron star binary systems. For heavier systems, like a system of two black holes, the final coalescence and even the ring down phases are in the LIGO frequency band. This is potentially very interesting from a scientific point of view, but the lack of detailed knowledge of the waveforms make the searches more challenging. The expected rate of coalescing binary neutron star systems (with large uncertainties) is expected to be a few per year within about 200 Mpc. Coalescence of neutron star/black hole or black hole/black hole airs may provide stronger signals but their rate of occurrence (as well as the required detection algorithms) are more uncertain. Recently, enhanced mechanisms for ~10M blackholeblackhole mergers have been proposed, making these systems of particular interest. The expected signal for different compact sources is indicated in Figure 5. Fig 5. The sensitivity curves for detection of compact binary inspirals for the initial and the improved LIGO interferometers are shown and compared with the expected signal from the neutron star – neutron star binary inspiral benchmark events. Note that the sensitivity of the initial detector has been chosen as a balance of the arguments above making detection plausible and the use of demonstrated technologies. Also shown is the sensitivity for 20 M blackhole mergers, showing the sensitivity to merger and ringdown phase. Periodic Signals Radiation from rotating non-axisymmetric neutron stars will produce periodic signals in the detectors. The emitted gravitational wave frequency is twice the rotation frequency. For many known pulsars, the frequency falls within the LIGO sensitivity band. Searches for signals from spinning neutron stars will involve tracking the system for many cycles, taking into account the doppler shift for the motion of the Earth around the Sun, and including the effects of spin-down of the pulsar. Both targeted searches for known pulsars and general sky searches are anticipated. Stochastic Signals Signals from gravitational waves emitted in the first instants of the early universe, as far back as the Planck epoch at 10-43 sec, can be detected through correlation of the background signals from two or more detectors. Gravitational waves can probe earlier in the history of the Universe than any other radiation due to the very weak 6 interaction. Some models of the early Universe can result in detectable signals. Observations of this early Universe gravitational radiation would provide an exciting new cosmological probe. Burst Signals The gravitational collapse of stars (e.g. supernovae) will lead to emission of gravitational radiation. Type I supernovae involve white dwarf stars and are not expected to yield substantial emission. However, Type II collapses can lead to strong radiation if the core collapse is sufficiently non-axisymmetric. The rate of Type II supernovae is roughly once every 30 years in our own Galaxy. This is actually a lower bound on the rate of stellar core collapses, since that rate estimate is determined from electromagnetic observations and some stellar core collapses could give only a small electromagnetic signal. The ejected mantle dominates the electromagnetic signal, while the gravitational wave signal is dominated by the dynamics of the collapsing core itself. Numerical modeling of the dynamics of core collapse and bounce has been used to make estimates of the strength and characteristics of the signal emitted in gravitational radiation. This is a very complicated problem and the predictions are quite model dependent, depending both on detailed hydrodynamic processes and the initial rotation rate of the degenerate stellar core before collapse. Estimating the event detection rate is consequently difficult and the rate may be as large as many per year with initial LIGO interferometers, or less than one per year with advanced LIGO interferometers. Probably a reasonable guess is that the initial detectors will not see far beyond our own galaxy, while an advanced detector should see out to the Virgo cluster, where the rate is a few/year. THE STATUS OF THE LIGO The construction of LIGO infrastructure in both Hanford, Washington and in Livingston, Louisiana began in 1996 and was completed on schedule at the end of last year. . The long beam pipes are kept under high vacuum at all times and can be isolated from the large chambers containing the mirror-test masses and associated optics and detectors by the means of large gate valves that allow opening the chambers without disturbing the vacuum in the long beam pipes (see Figure 6) The infrastructure for LIGO consists of prepartion of both sites, civil construction for both the laboratory buildings and the enclosures for the vacuum pipes, as well as the large volume high vacuum system to house the interferometers. The Fig. 6. A photograph of the large vacuum chambers large vacuum system was the most challenging part containing the various LIGO detector components is of the infrastructure for LIGO, involving 16 km or shown. These chambers are isolated from the long 1.2 m diameter high vacuum pipe. That system vacuum pipes by gate valves to access the equipment. achieved 10-6 torr vacuum pumping only from the ends with vacuum and turbo is in place and pumps. The long vacuum pipes were then ‘baked’ to accelerate the outgassing by wrapping the pipes in insulation and running a current of 2000 amps down the pipes, which raised the temperature to ~ 1600 C. We baked at this temperature for about one week. Following cooldown, the pipes have no leaks and achieved a vacuum of better than 10-9 torr. All 16 km of beam pipe are now under high vacuum and the level of vacuum achieved is such that noise from scattering off residual molecules should not be a problem for either initial LIGO or envisioned upgrades. The long beam pipes are kept under high vacuum at all times and can be isolated from the large chambers that contain the mirror-test masses and associated optics and detectors by the means of large gate valves that allow opening the chambers without disturbing the vacuum in the pipes. . Having completed the infrastructure, the installation and commissioning of the detector subsystems began this past year. The laser we have developed for LIGO is a 10W Nd:YAG laser at 1.064 m in the TEM00 mode. The laser has been developed for production through Lightwave Electronics, using their 700-mwatt NPRO laser as the input to a diode pumped power amplifier. This commercialized laser is now sold by Lightwave as a catalog item. 8 We have been running one laser continuously for about a year with good reliability. We are optimistic that this laser will make a reliable input light source for the LIGO interferometers. For the LIGO application, the laser must be further stabilized in frequency, power and pointing. We have developed a laser prestabalization subsystem, which is performing near our design requirements. We require for 40 Hz < f < 10 KHz, Frequency noise: Intensity noise: dn(f) < 10-2 Hz/Hz1/2 -6 1/2 dI(f)/I < 10 /Hz This low noise highly stabilized laser system has been tested and characterized in detail and is performing near LIGO design specifications. Figure 7 shows some performance measurements of the prestabilized laser system. Detailed characterization and improvement of noise sources continue . Fig 7. Performance of the LIGO prestabilized laser in frequency (left) and power (right). The lines indicate the noise requirements for the interferometers. The prestabilized laser beam is further conditioned by a 12 m triangular mode cleaner, which is also operational. The University of Florida group in LIGO has developed the input optics containing this mode cleaner. The beam has been successfully transported through that system and sent down the first 2 km arm. LIGO at Hanford has both a half-length (2km) and a full-length (4km) interferometer installed in the same vacuum chamber. The extra constraint of requiring a ½ size signal in the shorter interferometer will be used to eliminate common noise and lower the singles rate in the coincidence between the sites. Recently, the long 2 km arm cavities have been locked one at a time for typical few hour times, at which point lock is lost due to tidal effects. The electronics to compensate for tidal effects are not yet installed. This first success at locking a long cavity is an important accomplishment and gives us confidence we will soon lock the entire LIGO interferometer. Various monitoring signals for a 15 minute locked period are shown in Figure 8. The next and final step for the first interferometer, which we are using as a pathfinder to find any big problems, is to lock both arms at the same time, at which point we will have achieved the full LIGO suspended mass Michelson Interferometer with FabryPerot arms. Following the locking of the long arms early this year, The first step for us this summer was to turn on the power-recycled Michelson part of the interferometer, formed by the input mirrors, as well as the beam splitter and the recycling mirror. To make LIGO as sensitive as possible, we want to have as much light as possible returning to the beam splitter. This occurs when the recycling mirror is placed at the correct distance from the beam splitter, ‘trapping’ the reflected light in the Michelson interferometer. This causes the laser light in the interferometer to build up to a high level. For the full LIGO-I system, recycling will cause the light to build up by about a factor of thirty. When this build up occurs, the power-recycled Michelson interferometer is resonating. That resonant state was achieved within the last few weeks for this short arm system. We now plan to add one of the 2-km-long arms resonating, which will be the final step in preparation for turning on the full interferometer. We have now installed all of the electronics for the entire interferometer, and we expect to achieve ‘first lock’ of LIGO this fall. Fig 8. A locked stretch of a 2km arm of LIGO showing the transmitted light and various control and error signals is shown. This marks an important milestone in making LIGO operational. LIGO DATA ANALYSIS PREPARATIONS AND ISSUES We have been preparing for analysis of LIGO interferometer data. These preparartions have involved designing and implementing a computer system capable of LIGO data analysis, development and implementing algorithms for the different searches. In addition, we have been testing our ability to extract signals from noise expected in real interferometer data. I will only briefly discuss the last item here. Fig 9. An illustration is shown of the types of instrumental signals that must be dealt with in the LIGO interferometers. These are from the 40m prototype data. 1 0 In order to test the ability to pull signals out of real interferometer data, a test end-to-end analysis was performed using 40m data (noise curve is shown in Figure 4). The data taken in 1994 consists of a stretch of 44.8 hours of reasonably stable running. The data has been analyzed for neutron star binary inspirals using the technique of matched templates (a total of 687 filters). The sensitivity of the interferometer was h ~ 3.5 10-19 mHz-1/2, which corresponds to a sensitivity capable of making a detection within our galaxy, but not beyond. It should be noted that the expected rate in our galaxy is only ~10 -6/yr, so this data has a negligibly small chance for making a real detection. The real value is that it allows us to test how well the data analysis techniques work, in advance of obtaining real LIGO interferometer data. The data consists of 39.9 hrs of running where the interferometer was locked. This locked data was analyzed using good data segments within that data, which amounted to a reduction to 25.0 hrs of data (after removing obvious problems, sections too near the time lock was acquired, etc). For the LIGO interferometers, we hope to improve the fraction of good data available during a running period to at least 90%, and we have required such performance reliability in our interferometer design. It is important to note that the 40m interferometer data contains lots of features that that complicate the data analysis. Using such data provides a good test of our analysis. Some of the types of peculiar instrumental signals observed in the 40m data are shown in Figure 9. The data was first cleaned up using various procedures, for example removing sinusoidal artifacts by multi-taper methods. The data contains both significant non-stationary and non-gaussian noise, which we will need to deal with in LIGO data. In order to test how well one can extract a binary inspiral chirp signals from such noise, simulated events were superposed on the actual 40m noise and then the analysis code was used to extract the signal. The simulated signals covered the range of parameters for a binary system. A comparison then could be made of the efficiency of extracting these signals and how well the reconstructed parameters compared with the injected parameters (e.g. distance of the source). Figure 10 shows one such comparison by comparing the distance injected and reconstructed as a function of the distance. Perfect reconstruction would lie on the diagonal, so the deviation from that line is an indication of the error in reconstruction due to the presence of noise. It is clear that the events cluster quite well along the diagonal as desired. An analysis of the errors in distance measurements is consistent with the signal to noise ratio (SNR) fluctuations of our expectations. This demonstrates that the reconstruction of distance in the presence of this non-gaussian and non-stationary noise was not significantly degraded. From this data, an upper limit on event rate was determined using a technique based on the SNR of the ‘loudest’ event. The loudest event is the one that fit the template analysis best. From this analysis the limit on rate of binary inspirals in our galaxy was determined to be R < 0.5/hour with 90% CL. The overall detection efficiency = 0.33. It is worth noting that an ideal detector for this amount of good data would set a limit of R < 0.16/hour. From this study, we conclude that analysis for signals for binary inspirals works on Fig 10. Analysis of simulated events inserted into this within a factor of 3 degradation of what might be real 40m noise comparing the distance of the inserted expected in an ideal analysis. A challenge for us in event with the reconstructed distance from the data the development of the data analysis for the LIGO analysis interferometers is to improve this efficiency to be as close to the ideal case as possible. CONCLUSIONS AND PLANS We are optimistic that we will achieve the major milestone this year of locking the first full interferometer as a suspended mass Michelson interferometer with Fabry Perot arms. We will then characterize the performance and begin to concentrate our efforts on noise and reliability issues. We also will be commissioning the second and third interferometers, using lessons learned on the first interferometer. We expect to schedule some short engineering test runs during this long turn period. We already had one such engineering data run last March recording data for a single locked arm. We expect to have a similar short run once we lock the entire interferometer this fall and similarly another after we achieve coincidence running between the sites, probably by next summer. Our long-term plan is evolve into a science data-taking mode, where we suspend interferometer studies, and try to collect a significant amount of data some time during 2002. Our eventual goal to collect at least 1 year of integrated coincidence data between the two sites with sensitivity near 10 -21. Depending on how well we do at making LIGO robust and how quickly we obtain design noise levels, we estimate that goal should be reachable by sometime in 2005. As soon as possible following that achievement, we want to be prepared to undertake improvements that will yield a significant improvement in sensitivity. . As described above, the initial LIGO detector is a compromise between performance and technical risk. The design incorporates some educated guesses concerning the directions to take to achieve a reasonable probability for detection. It is a broadband system with modest optical power in the interferometer arms and a low risk vibration isolation system. The suspensions and other systems have a direct heritage to the demonstration interferometer prototypes we have tested over the last decade. As ambitious as the initial LIGO detectors seem, there are clear technical improvements we expect to make, following the initial search. The initial detector performance and results will guide the specific directions and priorities to implement from early data runs. We anticipate making both reductions of noise from stochastic sources and in the sensing noise. These improvements will include improvements in the suspension system to improve the thermal noise, the seismic isolation and improvements to the sensing noise through the use of higher power lasers in conjunction with improved optical materials for the test masses/mirrors to handle this higher power. We believe it is quite realistic to improve the sensitivity at 100 Hz by at least a factor of 10, and to broaden the sensitive bandwidth by about a factor without any radically new technologies or very large changes. This will improve the rate (or volume of the universe searched) at a fixed sensitivity by a factor of 1000. If the physics arguments favor an even greater sensitivity in a narrower bandwidth, it will be possible to change the optical configuration and make a narrow band device. In conclusion, I might note that over the next decade ground-based detectors offer good prospects for detection of gravitational waves. They are complementary in approach and in scientific coverage to space based detectors. Hopefully within about a decade we will be detecting signals from gravitational waves, both on the earh and in space. References 1. Barish, B.C. and R. Weiss, Physics Today, October 1999 and LIGO Web site http://www.ligo.caltech.edu/ 2. Thorne, K.S. 300 Years of Gravitation Edited by S.W. Hawking and W. Israel Cambridge University Press, Cambridge, England 1987 Chapter 9 “Gravitational radiation”
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