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Small Body Rendezvous Mission Using Solar Electric Ion Propulsion: Low Cost Mission Approach and Technology Requirements

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dc.contributor.author Kakuda, R. en_US
dc.contributor.author Sercel, J. en_US
dc.contributor.author Lee, W. en_US
dc.date.accessioned 2004-10-05T22:08:05Z
dc.date.available 2004-10-05T22:08:05Z
dc.date.issued 1994-04-12 en_US
dc.identifier.citation IAA International Conference on Low-Cost Planetary Missions en_US
dc.identifier.citation Laurel, Maryland, USA en_US
dc.identifier.clearanceno 94-0644 en_US
dc.identifier.uri http://hdl.handle.net/2014/33911
dc.description.abstract This paper shows that existing solar electric ion propulsion technology can deliver substantial payloads to important small bodies for an effective cost. en_US
dc.format.extent 938785 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other low-cost mission ion propulsion en_US
dc.title Small Body Rendezvous Mission Using Solar Electric Ion Propulsion: Low Cost Mission Approach and Technology Requirements en_US


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