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Additional historical solid rocket motor burns

delete2009-06-01
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PRE
AI
C
Carsten Wiedemann *
M
Maren Homeister
M
Michael Oswald
S
Sebastian Stabroth
H
H. Klinkrad
P
Peter Vörsmann
DOI:10.1016/j.actaastro.2009.01.011delete
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摘要

摘要

En 中文
The use of orbital solid rocket motors (SRM) is responsible for the release of a high number of slag and Al2O3 dust particles which contribute to the space debris environment. This contribution has been modeled for the ESA space debris model MASTER (Meteoroid and Space Debris Terrestrial Environment Reference). The current model version, MASTER-2005, is based on the simulation of 1076 orbital SRM firings which mainly contributed to the long-term debris environment. SRM firings on very low earth orbits which produce only short living particles are not considered. A comparison of the modeled flux with impact data from returned surfaces shows that the shape and quantity of the modeled SRM dust distribution matches that of recent Hubble Space Telescope (HST) solar array measurements very well. However, the absolute flux level for dust is under-predicted for some of the analyzed Long Duration Exposure Facility (LDEF) surfaces. This indicates that some past SRM firings are not included in the current event database. Thus it is necessary to investigate, if additional historical SRM burns, like the retro-bum of low orbiting re-entry capsules, may be responsible for these dust impacts. The most suitable candidates for these firings are the large number of SRM retro-bums of return capsules. This paper focuses on the SRM retro-bums of Russian photoreconnaissance satellites, which were used in high numbers during the time of the LDEF mission. It is discussed which types of satellites and motors may have been responsible for this historical contribution. Altogether, 870 additional SRM retro-bums have been identified. An important task is the identification of such missions to complete the current event data base. Different types of motors have been used to de-orbit both large satellites and small film return capsules. The results of simulation runs are presented. (C) 2009 Elsevier Ltd. All rights reserved.
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期刊

Acta Astronautica 封面图
Acta Astronautica
IF:
3.4
论文数:
1.2W
被引数:
2.1W

机构

E
European Space Agency
学者数:
5.4K
论文数: 4.0K
被引数: 518
B
Braunschweig University of Technology
学者数:
7.8K
论文数: 6.7K
被引数: 19
引用论文

引用论文

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