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Concept for a shuttle-tended reusable interplanetary transport vehicle using nuclear electric propulsion

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dc.contributor.author Nakagawa, R. Y. en_US
dc.contributor.author Elliot, J. C. en_US
dc.contributor.author Spilker, T. R. en_US
dc.contributor.author Grayson, C. M. en_US
dc.date.accessioned 2004-09-17T19:02:47Z
dc.date.available 2004-09-17T19:02:47Z
dc.date.issued 2003-03-08 en_US
dc.identifier.citation IEEE Aerospace Conference en_US
dc.identifier.citation Big Sky, MT, USA en_US
dc.identifier.clearanceno 02-2753 en_US
dc.identifier.uri http://hdl.handle.net/2014/10663
dc.description.abstract NASA has placed new emphasis on the development of advanced propulsion technologies including Nuclear Electric Propulsion (NEP). This technology would provide multiple benefits including high delta-V capability and high power for long duration spacecraft operations. en_US
dc.format.extent 4483556 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other interplanetary nuclear electric propulsion shuttle en_US
dc.title Concept for a shuttle-tended reusable interplanetary transport vehicle using nuclear electric propulsion en_US


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