DocumentCode
1150557
Title
New Power Processor Interfaces MMS Power Module Outputs
Author
Chetty, P.R.K.
Author_Institution
Fairchild Space Company
Issue
3
fYear
1987
fDate
5/1/1987 12:00:00 AM
Firstpage
311
Lastpage
316
Abstract
A description of a new power processor to interface the outputsfrom two or more multimission modular spacecraft (MMS) modularpower system (MPS) modules to the spacecraft payload is presented.Also included are an introduction describing the circumstances thatled to this power processor, and material concerning analysisresults, load programmability, and salient features, includingefficiency and weight aspects. Finally, important input and outputelectrical characteristics of this processor are summarized.
Keywords
Aircraft manufacture; Low earth orbit satellites; Military satellites; Multichip modules; NASA; Payloads; Power system reliability; Power system stability; Space technology; Space vehicles;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1987.310827
Filename
4104343
Link To Document