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
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