DocumentCode :
2109589
Title :
Emergency escape vehicles and mechanisms for space shuttles
Author :
Cheng, Shun-Wen
Volume :
4
fYear :
2004
fDate :
13-13 March 2004
Firstpage :
2631
Abstract :
This study considers emergency escape vehicles (EEV) design for Space Shuttles. The proposed EEV has the reverse Apollo-style cone configuration, contains a manned gyro-stabilized suspension rotator sphere, and has a collapsible module. Therefore, it gives astronauts a high permissible gravitational loading and survivability. The proposed EEV has high volumetric efficiency and is removable, so the Space Shuttle still can carry a large payload. The designs of the EEV system greatly extend the lifespan of the remaining space shuttle fleet indeed.
Keywords :
explosion protection; modules; space vehicles; Space Shuttles; collapsible module; emergency escape vehicles design; explosion protection; gravitational loading; manned gyro stabilized suspension rotator sphere; reverse Apollo style cone configuration; Aircraft; Aluminum; Earth; Equations; Explosives; Payloads; Space shuttles; Space technology; Space vehicles; Vehicle crash testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2004. Proceedings. 2004 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
0-7803-8155-6
Type :
conf
DOI :
10.1109/AERO.2004.1368058
Filename :
1368058
Link To Document :
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