VSOP-2 A next generation space-VLBI

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Check the system Design Structure Thermal Control Deformation Endurance of Vibration Radiation Mass budget Center of Mass Inertia Attitude Control Power budget etc
Expected Performance of ASTRO-G Based on the basic design, and BBM tests. • Freq. resolution SEFD 7-σ detection with VLBA 8 GHz 205 μas 6100 Jy 32 mJy 22 GHz 75 μas 3600 Jy 72 mJy 43 GHz 38 μas 7550 Jy 188 mJy Assumption • SEFD=2kTsys/Ae • Bandwidth for <strong>VSOP</strong>-2, 128 MHz /2bit or 256 MHz/1bit. ( Tsuboi et al. 2007 <strong>VSOP</strong>-2 Symposium @ Sagamihara)
Page 1 and 2: The VSOP-2 (ASTRO-G) Project Yasuhi
Page 3 and 4: VSOP with HALCA Beamwidth 100 Rs at
Page 5 and 6: Orbit : Apogee 25,000 km Perigee 1,
Page 7 and 8: Comparison of ASTRO-G/VSOP-2 and HA
Page 9 and 10: ASTRO-G Can see the root of the rel
Page 11: ASTRO-G Development schedule Financ
Page 15 and 16: Astro-G antenna performance based o
Page 17 and 18: Large Deployable Antennas (2/2) Imp
Page 19 and 20: Radio Quiet Room in JAXA Compact ra
Page 21 and 22: Receiver System 22GHz system •Dua
Page 23 and 24: ASTRO-G Observing System Engineerin
Page 25 and 26: Precision Oribt Determination BBM o
Page 27 and 28: VSOP-2 international collaborations
Page 29 and 30: European Astronomers and Space VLBI
Page 31 and 32: VSOP-2/Astro-G Tracking station mee
Page 33 and 34: VISC-2 • VISC-2 Formation - VISC-

VSOP-2 A next generation space-VLBI

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