The prelimary design of the propulsion subsystem for the CRAF and Cassini missions is described. It is noted that the propulsion module subsystem must provide impulse for a number of functions required by these missions. These functions include the acquisition of celestial references and trajectory correction maneuvers. A schedule for the CRAF/Cassini Project is provided.
The CRAF/Cassini spacecraft propulsion subsystem - A preliminary design
1991-06-01
Conference paper
No indication
English
AIAA | 1990
|NTRS | 1990
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