DocumentCode :
827314
Title :
Low Power CAMAC and NIM Modular Systems for Spaceflight Use on Shuttle and Spacelab Missions
Author :
Trainor, James H. ; Kaminski, Thomas J. ; Ehrmann, Charles H.
Author_Institution :
NASA/Goddard Space Flight Center Greenbelt, Maryland 20771
Volume :
24
Issue :
1
fYear :
1977
Firstpage :
835
Lastpage :
839
Abstract :
The advent of the Shuttle launch vehicle and Spacelab have resulted in adequate weight and volume such that experiment electronics can be implemented at relatively low cost using spaceflight versions of CAMAC and NIM modules. Studies of 10 modules by manufacturers have shown that power reduction overall by a factor of ~ 3 can be accomplished. This is adequate both from the point of view of consumption and temperature rise in vacuum. Our studies have shown that a stock of ~ 45 module types is required and a listing is given. The changes required in these modules in order to produce spaceflight versions are described. And finally, the further studies, prototyping and testing leading to eventual flight qualification are described.
Keywords :
Acoustical engineering; Aerospace engineering; CAMAC; NASA; Payloads; Satellites; Space missions; Space shuttles; Space vehicles; Testing;
fLanguage :
English
Journal_Title :
Nuclear Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9499
Type :
jour
DOI :
10.1109/TNS.1977.4328790
Filename :
4328790
Link To Document :
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