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
Link To Document :
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