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The Mars Exploration Rovers entry descent and landing and the use of aerodynamic decelerators

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dc.contributor.author Steltzner, A. en_US
dc.contributor.author Desai, P. en_US
dc.contributor.author Lee, W. en_US
dc.contributor.author Bruno, R. en_US
dc.date.accessioned 2004-09-16T23:09:51Z
dc.date.available 2004-09-16T23:09:51Z
dc.date.issued 2003-05-20 en_US
dc.identifier.citation Aerodynamic Decelerators Conference en_US
dc.identifier.citation Monterey, CA, USA en_US
dc.identifier.clearanceno 03-1306 en_US
dc.identifier.uri http://hdl.handle.net/2014/7442
dc.description.abstract The Mars Exploration Rovers (MER) project, the next United States mission to the surface of Mars, uses extensive aerodynamic deceleration in during its entry, descent and landing (EDL) phase. en_US
dc.format.extent 3065081 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other EDL MER entry descent landing Mars en_US
dc.title The Mars Exploration Rovers entry descent and landing and the use of aerodynamic decelerators en_US


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