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Attitude Control of the Cassini Spacecraft During Propulsive Maneuvers

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dc.contributor.author Enright, P.J. en_US
dc.date.accessioned 2004-10-06T04:40:29Z
dc.date.available 2004-10-06T04:40:29Z
dc.date.issued 1993-08-16 en_US
dc.identifier.citation Victoria, B.C., Canada en_US
dc.identifier.clearanceno 93-1439 en_US
dc.identifier.uri http://hdl.handle.net/2014/35714
dc.description.abstract The Saturn-bound Cassini spacecraft performs trajectory correction maneuvers using either the 0.6 N Hydrazine thrusters of the reaction control system (RCS) or one of the two gimbaled 490 N bipropellant main engines. en_US
dc.format.extent 954847 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Attitude Control Cassini en_US
dc.title Attitude Control of the Cassini Spacecraft During Propulsive Maneuvers en_US


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