发明名称 |
SOLID ROCKET MOTOR BOLTED THRUST TAKEOUT STRUCTURE |
摘要 |
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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申请公布号 |
US2003015623(A1) |
申请公布日期 |
2003.01.23 |
申请号 |
US20010910440 |
申请日期 |
2001.07.19 |
申请人 |
AEROJET-GENERAL CORPORATION |
发明人 |
GLADSTONE JEFFREY D.;MOURITSEN JOHN |
分类号 |
B64G1/00;B64G1/64;(IPC1-7):B64D27/00 |
主分类号 |
B64G1/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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