Solid rocket motor bolted thrust takeout structure
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United States of America Patent
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-
Apr 15, 2003
Grant Date -
Jan 23, 2003
app pub date -
Jul 19, 2001
filing date -
Jul 19, 2001
priority date (Note) -
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Abstract
A solid rocket motor used as a booster rocket for a launch vehicle is provided with a mounting structure that permits attachment of the rocket motor to the vehicle in a manner that accommodates the expansion that the rocket undergoes during firing without risking disengagement of the rocket due to the shear forces caused by the expansion. The mounting structure includes a raised hub to which the thrust pin is attached, a series of aft-directed struts and a pair of transverse struts, all terminating in separate plates for bolting to the rocket motor case.
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