The radar payload on a space-based radar (SBR) satellite could require tens of kilowatts of power distributed to many small loads over a large area. This poses special problems for the power distribution and control system (PDCS). A study that examined the power requirements of an SBR spacecraft is reported. A baseline prime power system, generating about 30 kW, was derived. The proposed distribution network would transmit 240 V at 20 kHz. The voltage would be downconverted in one converter for about 100 transmit/receive modules. The design considerations are discussed, and the baseline PDCS is described.
Electrical power distribution on space based radar satellites
Elektrische Energieversorgung für Radarsatelliten im Raum
IEEE Aerospace and Electronics Systems Magazine ; 4 , 11 ; 10-16
1989
7 Seiten, 9 Quellen
Aufsatz (Zeitschrift)
Englisch
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