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    Development of a bipropellant propulsion module for the Galileo spacecraft (1984)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: The bipropellant engine retropropulsion module (RPM) of the Jupiter-exploration Galileo spacecraft provides attitude control, trajectory correction, a deep space velocity increment, a spacecraft deflection maneuver for an entry capsule, a retromaneuver for Jupiter approach, and a 'perijove raise' maneuver for the Jovian system tour of the spacecraft. Attention is given to the design features and performance capabilities of the RPM, which uses a set of 12 10-N thrusters in conjunction with a 400-N engine. Tanks contain 935 kg of propellant to satisfy mission requirements.
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: AIAA PAPER 84-1233
    Format: text
    Location Call Number Expected Availability
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