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.
Attitude Control of the Cassini Spacecraft During Propulsive Maneuvers
1993-08-16
Preprint
Keine Angabe
Englisch
Attitude Control of the Cassini Spacecraft During Propulsive Maneuvers
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