DocumentCode
2203150
Title
Study on Vulnerability Model of Spacecraft Impacting by Orbital Debris
Author
LIU, Chunmei ; FENG, Shunshan ; ZHANG, Xurong
Author_Institution
State Key Lab. of Explosion Sci. & Technol., Beijing Inst. of Technol., Beijing, China
fYear
2008
fDate
20-22 Dec. 2008
Firstpage
1067
Lastpage
1070
Abstract
The spacecraft was studied. Spacecraft vulnerability was analyzed in some aspects as environment, representative structure, aviation theory, damage principle and existence speciality. Then the destruction types were advanced on debris against double plates. The damage types included local perforation and avulsion. And the respective lethality model was put forward. At last the damage probability was obtained when one fragment impacts the double boards by hypervelocity. It is a certain reference and important reality signification, that the vulnerability analysis and lethality mathematical model of spacecraft are researched, to strengthen our space defense ability.
Keywords
aerospace safety; probability; space debris; space vehicles; aviation theory; damage probability; destruction type; hypervelocity; lethality model; orbital debris; representative structure; spacecraft existence speciality; spacecraft vulnerability model; work environment; Aerodynamics; Aircraft manufacture; Airplanes; Control systems; Engines; Gravity; Satellites; Space debris; Space vehicles; Vehicle detection; damage probability; orbital debris; spacecraft; vulnerability mathematics model;
fLanguage
English
Publisher
ieee
Conference_Titel
Advanced Computer Theory and Engineering, 2008. ICACTE '08. International Conference on
Conference_Location
Phuket
Print_ISBN
978-0-7695-3489-3
Type
conf
DOI
10.1109/ICACTE.2008.103
Filename
4737121
Link To Document