DocumentCode :
2839125
Title :
Space application of airborne common modules
Author :
Flanagan, R.A. ; Mosher, T.O. ; Fleischman, D.L. ; Bond, D.G.
Author_Institution :
Boeing Defense & Space Group, Seattle, WA, USA
fYear :
1991
fDate :
14-17 Oct 1991
Firstpage :
26
Lastpage :
31
Abstract :
It is shown that, with some early planning, common electronics modules designed for combat aircraft can be used in space applications. It is shown that architectures, made up of common modules, can be constructed in a manner that resolves reliability, safety, environmental and cost concerns. Growth path and capability are shown for near-term projects (heavy launch vehicle) through far-term (manned Mars mission) applications. Performance requirements, environmental specifications, validation methods, and testing philosophy for missions in space transportation are addressed
Keywords :
aerospace instrumentation; modules; reliability; safety; space vehicles; airborne common modules; common electronics modules; cost concerns; environmental concerns; heavy launch vehicle; manned Mars mission; performance requirements; reliability; safety; validation methods; Acoustic testing; Aerospace electronics; Application software; Costs; Hardware; Mars; Space missions; Space technology; Space vehicles; Transportation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 1991. Proceedings., IEEE/AIAA 10th
Conference_Location :
Los Angeles, CA
Type :
conf
DOI :
10.1109/DASC.1991.177139
Filename :
177139
Link To Document :
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