Photographic and Radiometric Observations of the HAYABUSA Re-Entry

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, i...

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Main Authors: Borovicka, J., Abe, S., Shrbený, L., Spurney, P., Bland, Phil
Format: Journal Article
Published: Nihon Tenmon Gakkai 2011
Subjects:
Online Access:http://hdl.handle.net/20.500.11937/36289
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author Borovicka, J.
Abe, S.
Shrbený, L.
Spurney, P.
Bland, Phil
author_facet Borovicka, J.
Abe, S.
Shrbený, L.
Spurney, P.
Bland, Phil
author_sort Borovicka, J.
building Curtin Institutional Repository
collection Online Access
description 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 m s −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.
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spelling curtin-20.500.11937-362892017-09-13T15:22:42Z Photographic and Radiometric Observations of the HAYABUSA Re-Entry Borovicka, J. Abe, S. Shrbený, L. Spurney, P. Bland, Phil meteors meteorites astrometry space vehicles: individual (HAYABUSA) meteoroids 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 m s −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. 2011 Journal Article http://hdl.handle.net/20.500.11937/36289 10.1093/pasj/63.5.1003 Nihon Tenmon Gakkai unknown
spellingShingle meteors
meteorites
astrometry
space vehicles: individual (HAYABUSA)
meteoroids
Borovicka, J.
Abe, S.
Shrbený, L.
Spurney, P.
Bland, Phil
Photographic and Radiometric Observations of the HAYABUSA Re-Entry
title Photographic and Radiometric Observations of the HAYABUSA Re-Entry
title_full Photographic and Radiometric Observations of the HAYABUSA Re-Entry
title_fullStr Photographic and Radiometric Observations of the HAYABUSA Re-Entry
title_full_unstemmed Photographic and Radiometric Observations of the HAYABUSA Re-Entry
title_short Photographic and Radiometric Observations of the HAYABUSA Re-Entry
title_sort photographic and radiometric observations of the hayabusa re-entry
topic meteors
meteorites
astrometry
space vehicles: individual (HAYABUSA)
meteoroids
url http://hdl.handle.net/20.500.11937/36289