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