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.
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
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