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A Summary of Thermal Analysis Support to the Galileo High Gain Antenna Deployment Anomaly Recovery Effort

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dc.contributor.author Tsuyuki, G. en_US
dc.contributor.author Reeve, R. en_US
dc.date.accessioned 2004-10-06
dc.date.available 2004-10-06
dc.date.issued 1994--June en_US
dc.identifier.citation Colorado Springs, Colorado, USA en_US
dc.identifier.clearanceno 94-0908 en_US
dc.identifier.uri http://hdl.handle.net/2014/34557
dc.description.abstract In April of 1991, the Galileo spacecraft executed a sequence of commands to unfurl its unbrella-like high gain antenna. After analysis of flight telemetry and ground testing of the spare antenna, indications were that three or four of the eighteen antenna ribs were struck in their stowed position. en_US
dc.format.extent 899760 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Galileo spacecraft umbrella-like high gain antenna friction mechanical hammer en_US
dc.title A Summary of Thermal Analysis Support to the Galileo High Gain Antenna Deployment Anomaly Recovery Effort en_US


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