Bounding the risk of crew loss following orbital debris penetration of the international space station at assembly stages 1J and 1E-Reference-Cited by-同舟云学术

Bounding the risk of crew loss following orbital debris penetration of the international space station at assembly stages 1J and 1E

Published:2004-01 Issue:5 Volume:34 Page:1104-1108
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Evans S.,Lewis H.,Williamsen J.,Evans H.,Bohl W.

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference9 articles.

1. Alibaruho, Q. Private communications, February 2000 and August 2001

2. Berdich, M. Private communications, February 2000 and August 2001

3. Kessler, D.J., Zhang, J., Matney M.J., et al. A Computer Based Orbital Debris Model for Spacecraft Design and Observation in Low Earth Orbit, NASA Technical Memorandum TM 104825, November 1996

4. Lamczyk, P. Private communications, February 2000 and August 2001

5. Lee, R. Private communication, August 2001

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