Method for satellite injection using a solid fuel rocket motor
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United States of America Patent
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Nov 13, 2001
Grant Date -
N/A
app pub date -
Feb 10, 2000
filing date -
Feb 10, 2000
priority date (Note) -
Expired
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Abstract
A method of injecting a missile, having a solid fuel motor, into a satellite orbit. The method includes determining an along-track displacement and cross-track displacement with respect to the satellite orbit. The method also includes determining a velocity-to-be-gained for the satellite orbit, with respect to the current missile velocity. Along-track and cross-track wasting of the solid fuel motor are used to reach the satellite orbit, at the proper velocity for the satellite orbit, when the solid fuel motor burns out.
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