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Attitude Control of the Cassini Spacecraft During Propulsive ManeuversThe 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.
Document ID
20060039254
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/35714
Authors
Enright, P. J.
Date Acquired
August 23, 2013
Publication Date
August 16, 1993
Subject Category
Astrodynamics
Distribution Limits
Public
Copyright
Other
Keywords
Attitude Control Cassini

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