JPL Technical Report Server

Evaluation of Cryogenic Power Conditioning Subsystems for Electric Propulsion Spacecraft

Show simple item record

dc.contributor.author Das, R. en_US
dc.contributor.author Krauthamer, S. en_US
dc.contributor.author Frisbee, R. en_US
dc.date.accessioned 2004-09-30T22:20:50Z
dc.date.available 2004-09-30T22:20:50Z
dc.date.issued 1996-08-11 en_US
dc.identifier.citation Washington, D.C., USA en_US
dc.identifier.clearanceno 96-1013 en_US
dc.identifier.uri http://hdl.handle.net/2014/26006
dc.description.abstract The power requirement of vehciles desgined to transport cargo supporting a piloted expedition to Mars is in the range of megawatts. Therefore, it is imperative that the megawatt - class power processing unit designed for high-power nuclear electric propulsion vehicles using turboalternators and advanced magnetoplasmadynamic thrusters shouls be such that the overall system efficienty is as high as possible with minimum system specific mass. en_US
dc.format.extent 634757 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other cryogenic power electric propulsion spacecraft en_US
dc.title Evaluation of Cryogenic Power Conditioning Subsystems for Electric Propulsion Spacecraft en_US


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search


Browse

My Account