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dc.contributor.author Matousek, S. en_US
dc.contributor.author Leschly, K. en_US
dc.contributor.author Gershman, B. en_US
dc.contributor.author Reimer, J. en_US
dc.date.accessioned 2004-09-24T16:26:48Z
dc.date.available 2004-09-24T16:26:48Z
dc.date.issued 1999-08-23 en_US
dc.identifier.citation 13th USU/AIAA Smallsat Conference en_US
dc.identifier.citation Logan, Utah, USA en_US
dc.identifier.clearanceno 99-1262 en_US
dc.identifier.uri http://hdl.handle.net/2014/17812
dc.description.abstract A Mars micromission launches as an Ariane 5 secondary as early as November 1, 2002. One possible mission is a comm/nav micromission orbiter. The other possible mission is a Mars airplane. Both missions are enabled by a low-cost, common micromission bus design. en_US
dc.format.extent 806947 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Mars Micromissions Secondary Payload Venus Mercury en_US
dc.title Mars Micromissions en_US


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