DocumentCode
2175235
Title
Power conditioning requirements and trade-off considerations for the space shuttle
Author
Collins, W.B. ; Newell, D.R.
Author_Institution
Denver Div., Martin Marietta Corp., Denver, CO, USA
fYear
1971
fDate
19-20 April 1971
Firstpage
5
Lastpage
12
Abstract
Avionics equipment that utilize electrical power typically convert this power by means of a converter internal to the equipment into several voltage levels. These voltages are regulated and used to power the electronic circuits within the equipment. Considering the number of electronics equipments required on the shuttle, the question arises as to whether the power converter normally supplied in each electronics equipment could be combined into a central power converter. A power distribution system would then distribute the various voltages to each load as required.
Keywords
avionics; space vehicle power plants; avionics equipment; central power converter; electrical power utilization; power conditioning requirements; power distribution system; space shuttle; trade-off considerations; Circuit breakers; Electronic equipment; Power conditioning; Power distribution; Vehicles; Wires;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Electronics Specialists Conference, 1971 IEEE
Conference_Location
Pasadena, CA
ISSN
0275-9306
Type
conf
DOI
10.1109/PESC.1971.7069128
Filename
7069128
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