This paper proposes a novel electrical power supply system architecture (power conditioning and processing unit, PCPU) for high-power all-electric propulsion spacecraft platform with high-voltage power bus (HVBUS) powering thrusters and regulated power bus (VBUS) powering onboard payloads, respectively. The design principle of function modules in PCPU has been analyzed. Besides, the test on electrical characteristic of VBUS and HVBUS in prototyped system proves the stable and reliable work of buses in PCPU.
New Electrical Power Supply System for All-Electric Propulsion Spacecraft
IEEE Transactions on Aerospace and Electronic Systems ; 53 , 5 ; 2157-2166
2017-10-01
931333 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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Electric Propulsion of Spacecraft
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|Spacecraft electric propulsion - Now?
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