Publication of the Astronomical Society of Japan 63, 1003–1009 (2011)
Photographic and Radiometric Observations of the HAYABUSA Re-Entry
Jiri Borovicka1, Shinsuke Abe2,
Lukas Shrbeny1, Pavel
Spurny1, Philip A. Bland3
1Astronomical Institute of the
Academy of
Sciences, Fricova 298, CZ-25165 Ondrejov Observatory, Czech Republic
2Institute of Astronomy, National Central University,
300 Jhongda Road, Jhongli, Taoyuan, 32001, Taiwan
3IARC, Department of Earth Science and Engineering, Imperial
College London, London SW7 2AZ, UK
Abstract.
We analyzed photographic observations of the re-entry of the HAYABUSA
spacecraft and capsule over Southern Australia on 2010 June 13, 13:52
UT. Radiometric measurements of the brightness of the associated
fireball were obtained as well. We derived the trajectories and
velocities of the spacecraft, its four fragments, and the capsule. The
capsule trajectory was within a few hundred meters of the trajectory
predicted by JAXA prior to re-entry. The spacecraft trajectory was
about 1 km higher than the capsule trajectory. Two major fragments
separated from the spacecraft at a height of about 62 km with a mutual
lateral velocity of 250 ms-1. The maximum absolute magnitude
of the fireball of –12.6 was reached at a height of 67 km. The dynamic
pressures acting on the spacecraft at the fragmentation points were
only 1–50 kPa. No spacecraft fragment was seen to survive below a
height of 47 km. The
integral luminous efficiency of the event was 1.3%. As expected, the
capsule had a very low luminous efficiency and very low ablation
coefficient. The ablation coefficients and masses of the major
spacecraft fragments are discussed.
Keywords: astrometry— Meteors, meteoroids— space vehicles:
individual (HAYABUSA)
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