DocumentCode
1180240
Title
Line Replaceable Unit (LRU) Analysis in the Space Shuttle Orbiter Electrical Power System
Author
Oepomo, Tedja Santanoe
Author_Institution
Space Transportation and Systems Group Rockwell International
Issue
12
fYear
1985
Firstpage
3501
Lastpage
3509
Abstract
The National Aeronautics and Space Administration (NASA) Space Shuttle orbiter, as a test bed for low-orbit space laboratory experiments, needs an orbiter voltage analysis on all orbiter line replaceable units (LRU´s). This analysis should use a mathematical model to predict voltages at the various LRU´s so that voltage drops from a bus to an LRU can then be computed based on calculated resistance of the conductors and load current.
Keywords
Conductors; Laboratories; Mathematical model; NASA; Orbital calculations; Power system analysis computing; Power system modeling; Space shuttles; Testing; Voltage;
fLanguage
English
Journal_Title
Power Apparatus and Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9510
Type
jour
DOI
10.1109/TPAS.1985.318902
Filename
4113049
Link To Document