发明名称 Orbital assist module and interstage
摘要 An orbital assist module and an interstage for a launch vehicle. The orbital assist module includes a cylindrical outer wall and a support structure secured to an inner surface of the cylindrical outer wall. The support structure defines a plurality of fuel tank supporting zones, at least one of the zones supporting a fuel tank by means of securing formations. A plurality of nozzles are connected to the fuel tanks by means of fuel lines and a plurality of valves are mounted in the fuel lines. The interstage comprises a cylinder having a leading and a trailing end and an explosive connector at the leading end for connecting the interstage to a trailing end of a launch vehicle motor. A connecting bracket is secured to the trailing end of the cylinder for connecting a second launch vehicle motor to the cylinder.
申请公布号 US5816539(A) 申请公布日期 1998.10.06
申请号 US19950511346 申请日期 1995.08.04
申请人 LOCKHEED MARTIN CORPORATION 发明人 CHAN, ALLAN L.;CONNORS, JAMES J.;EPSTEIN, KENNETH W.;HEATH, ROBERT M.;OGDEN, GENE SPENCER;PREWITT, MICHAEL B.;WONG, MICHAEL;SZETO, EDWARD W.;KENNON, DAVID P.;VOGEL, MICHAEL J.;HSU, LARRY Y.;HADA, DANIEL H.;PEREYDA, DOUGLAS B.;MACDONALD, ROBERT J.
分类号 B64F1/04;B64G1/00;B64G1/40;B64G1/64;B64G5/00;F02K9/34;(IPC1-7):B64G1/40;B64G1/42;F02K9/00;B64D37/04 主分类号 B64F1/04
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