Solar Radiophysics with HF Radar Workshop on Solar Radiophysics With the Frequency Agile Solar Radiotelescope (FASR) 23-25 May 2002 Green Bank, WV Paul Rodriguez Information Technology Division Naval Research Laboratory Washington, DC The Solar & Lunar HAARP Radial Distance 1 AU 0.5 AU Range of Space Experiments with HF Radiowaves Solar Corona Detection of CMEs & prediction of geomagnetic storms Densities, temperatures of solar corona Large scale structure, dynamics, wave spectrum Planetary Surfaces Detection of near earth asteroids, comets 60 Re 30 Re Selenosphere Lunar surface penetration by HF radiowaves Charged lunar dust atmosphere? Lunar wake structure Solar Wind Solar wind large scale density structures Bow shock irregularities and dynamics 15 Re Magnetosphere 0.05 Re Ionosphere Boundary and global scale dynamics Response to geomagnetic storms Magnetospheric wave-particle interactions Modification (growth and decay scales of irregularities) Long distance radiowave propagation Density irregularity spectrum Meteor showers (Leonids; dusty plasmas) 0.1 MW 1 MW 10 MW 100 MW Effective Radiated Power 1000 MW El Campo, Texas Solar Radar Antenna Array Operated by MIT/Lincoln Laboratory 1961-1969 S E W N Operating Frequency: Transmitting Dipoles: Receiving Dipoles: 38.25 MHz 128 x 8 EW 128 x 8 EW 128 x 4 NS Total Area: 18,000 m2 Antenna Gain: 32-36 dB Beam Size (NS x EW): 1o x 6 o Total Power: 500 kW Effect. Radiated Power: 1300 MW Motivation for initial solar radar experiments • to determine radar cross section of the solar corona (however, it was recognized there was no ‘hard surface’ ) • to investigate dynamics of solar corona Present scientific motivation • profile of corona electron density • backscatter from a hot, magnetized plasma • remote sensing of wave-particle interactions in the corona (small scale dynamics) • measurement of large scale MHD (i.e., CMEs) • understanding of nonthermal development of various spectra (density fluctuations, waves, radio, etc) • direct measurements of stellar plasma and how it affects planetary environment Solar Radar Performance The radar equation is Pt Gt Pr = where: 4πR Pr Pt Gt Ar - Ar σ p 2 4πR received power (watts) transmitted power (watts) transmitting antenna gain receiving antenna area (m2) 2 σ - scattering cross-section (m2) p - polarization fraction R - range to scattering cross-section (m) Ro - solar radius (m) R = 1.5 x 1011 m (1 AU) Ro = 7 x 108 m (solar radius) σ ~ 1 π Ro2 = 1.54 x 1018 m2 ( typical value obtained by El Campo) p = 0.5 (one of two polarizations) N = kB T(f) B (noise power of sun), where kB = 1.38 x 10-23 watt-s °K-1 (Boltzman’s constant) T(f) = noise equivalent temperature of sun (°K) B = receiver bandwidth (Hz) El Campo Solar Radar (38.25 MHz) 40 o 2 Cross Section (πR ) 50 30 20 10 0 21000 21500 22000 22500 23000 23500 24000 30 Jun 61 12 Nov 62 26 Mar 64 8 Aug 65 21 Dec 66 4 May 68 16 Sep 69 Serial Day Day Month Year El Campo Corona Echo Signal Spectrum Typical RDA spectrum. Among spectral types observed were “high corona echoes,” which may have been CME signatures. However, CMEs were unknown in the 1960s. Solar Radar Detection of Earthward-Directed Coronal Mass Ejections CME Solar Radar Transmitted Power Received Corona CME Frequency Shift HF Doppler Shift from Earthward Motion of Coronal Mass Ejection 400 Frequency Shift (kHz) f Dp (9 MHz) f Dp (25 MHz) f Dp (38 MHz) 300 200 100 0 0 200 400 600 800 1000 1200 1400 1600 CME Velocity (km/s) The Doppler shifts expected for HF radar frequencies of 9, 25, and 38 MHz, for the range of CME velocities observed with coronagraphs. Solar Radar Experiment 21 July 1996 8.920 MHz Full Power ON/ OFF 10 SURA Transmitted Signal UT 0911-0927 20 30 40 50 60 seconds 40 50 60 seconds 8.880 MHz 0 10 20 30 UTR-2 Return Signal Spectra UT 0927-0943 44 Frequency Shift (kHz) 8.925 MHz 0 -10 OFF 0 ON 10 -10 ON 0 OFF 10 44 Frequency Shift (kHz) 8.885 MHz 0 Time (sec) Relative to Transition Integrated Return Signal Time Profiles and Spectra SURA / UTR-2 10 8.885 MHz Relative Intensity 21 July 1996 Transmission Patterns 8.925 MHz ON 8 OFF 6 4 ON OFF 2 0 -10 -5 SURA / UTR-2 Relative Spectral Intensity Solar Radar 0 Time (sec) Solar Radar 5 10 21 July 1996 6500 8.925 spec 8.885 spec 6000 5500 5000 4500 0 5 Receiver Frequency 10 15 20 25 30 35 Frequency Shift (kHz) 40 HAARP Research Facility Gakona, Alaska Operated by Advanced Power Technologies, Inc. under contract from U. S. Air Force/ Navy Current Radiating x-dipoles: 48 Total area (m2): 20,000 Transmitters: 96 Power (kW): 960 ERP (MW): 190 Frequencies (MHz): 2.8 to 8 Design 180 124,000 360 3600 3200 2.8 to 10 Sun As Seen From HAARP at UT 2000 (o), 2100 (◊), 2200 (∆), 2300 (x) LT 1100 (o), 1200 (◊), 1300 (∆), 1400 (x) 90 80 Altitude (deg) 70 Solar Radar Window 60 50 40 30 20 10 Jan Feb Mar Apr May Jun Jul Aug Sep Oct Nov Dec 0 30 61 91 122 152 182 213 243 274 304 335 365 Day of Year (2000) LOFAR: CONCEPTUAL LAYOUT LOFAR will be: ~ 1 meter Active dipole • ≥ 40 stations Los Alamos • ≥ 10,000 dipoles • ≥ 1 km2 collecting area – 20x Arecibo Ground Screen VLA Each LOFAR Station consists of 256 Active Dipoles above their ground screens ~ 160 m (5 acres) • ∆ν ~ 10-250 MHz • ≥ 2 independent beams New Mexico Possible LOFAR Station sites HALO Solar Radar 30 HAARP Frequency = 10 MHz Net Signal/Noise Ratio (dB) 25 LOFAR Effective Area ~ 106 m 2 Solar Radar X-Section = 1 20 Total Power (MW) 15 10 3.2 5-dB Threshold 5 0 0.9 -5 Initial HAARP Power 0.3 -10 0. 1 Present HAARP Power Design HAARP Power 10 100 Integration Time (s) 1000 10000 Summary and Conclusions • Solar radar experiments will ‘open’ a new window on plasma physics of the sun and magnetosphere. • Solar radar has applications to many other phenomena of local astrophysics. • HAARP is capable of being a solar radar, in bistatic configuration with existing and planned receiving arrays. • The CME detection problem and geomagnetic storm effects at earth is a practical motivating issue.
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