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Test Verification of the Cassini Spacecraft Dynamic Model

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dc.contributor.author Coleman, Michelle en_US
dc.contributor.author Peng, Chia-Yen en_US
dc.contributor.author Smith, Kenneth S. en_US
dc.date.accessioned 2004-10-01T06:17:02Z
dc.date.available 2004-10-01T06:17:02Z
dc.date.issued 1997-02-01 en_US
dc.identifier.citation Aspen, CO en_US
dc.identifier.clearanceno 96-1752 en_US
dc.identifier.uri http://hdl.handle.net/2014/27685
dc.description.abstract The Cassini spacecraft mission to Saturn will be launched in October 1997, on a Titan IV/Centaur launch vehicle. Cassini is the largest interplanetary spacecraft ever developed. Before launch approval can be obtained, a test verified finite element model of the Cassini spacecraft must be completed and approved by NASA. The correctness of this model is critical to the final verification coupled loads analysis and margin of safety assessments. en_US
dc.format.extent 381100 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Cassini test verification modal testing loads analysis finite element models nondestructive testing structural testing static testing dynamic testing vibration testing en_US
dc.title Test Verification of the Cassini Spacecraft Dynamic Model en_US


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