Geostationary earth observation satellite incorporating multiple thruster liquid propellant apogee maneuver system
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United States of America Patent
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Jul 24, 2001
Grant Date -
N/A
app pub date -
Sep 8, 1999
filing date -
Feb 26, 1990
priority date (Note) -
Expired
status (Latency Note)
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Abstract
A satellite designed to be spin-stabilized in geostationary orbit which has, coaxial with a spin rotation axis, a satellite body surrounded with a cylindrical solar generator, an apogee maneuver system disposed along the axis and two axially disposed equipments. The apogee maneuver system has opposite one of the equipments at least two thrusters oriented parallel to the axis but offset relative thereto by the same distance. Equi-angularly spaced around the other of the two equipments, the thrusters are connected to a common liquid propellant feed system.
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