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Mars 2001 Aerobot/Balloon System Overview

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dc.contributor.author Nock, K. T. en_US
dc.contributor.author Balaram, J. en_US
dc.contributor.author Heun, M. K. en_US
dc.contributor.author Smith, I. S. en_US
dc.contributor.author Gamber, T. en_US
dc.date.accessioned 2004-09-26
dc.date.available 2004-09-26
dc.date.issued 1997-06-03 en_US
dc.identifier.citation San Francisco, California, USA en_US
dc.identifier.clearanceno 97-0656 en_US
dc.identifier.uri http://hdl.handle.net/2014/22192
dc.description.abstract The purpose of the study was to determine technical feasibiltiy of a long duration 2001 aerobot mission in the Martian atmosphere, to formulate a baseline concept, to identify pre-project technology requirements and to develop a preliminary cost, schedule and plan. en_US
dc.format.extent 417678 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Mars Aerobot/Balloon System en_US
dc.title Mars 2001 Aerobot/Balloon System Overview en_US


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