JPL Technical Report Server

Model Correlation for Mars Pathfinder Entry, Descent and Landing Simulation

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dc.contributor.author Peng, C. Y. en_US
dc.contributor.author Tsang, S. K. en_US
dc.contributor.author Smith, K. en_US
dc.contributor.author Sabahi, D. en_US
dc.contributor.author Short, K. en_US
dc.contributor.author Mauritz, A. en_US
dc.date.accessioned 2004-10-01T06:17:17Z
dc.date.available 2004-10-01T06:17:17Z
dc.date.issued 1997-02-01 en_US
dc.identifier.citation Aspen, Colorado, USA en_US
dc.identifier.clearanceno 96-1755 en_US
dc.identifier.uri http://hdl.handle.net/2014/27687
dc.description.abstract Two multi-body drop tests were conducted to provide data to calibrate and verify a multi-body dynamics computer model, which was the major analytical tool used to study the entry, descent and landing (EDL) of the Mars Pathfinder mission. A general summary of the tests and important features of the simulation model are presented in this paper. Good correlation between between test results and analytical predictions were achieved. en_US
dc.format.extent 1223650 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Mars Pathfinder Mars Pathfinder EDL Mars Pathfinder drop tests drop tests EDL en_US
dc.title Model Correlation for Mars Pathfinder Entry, Descent and Landing Simulation en_US


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