发明名称 Load-reducing rocket nozzle operation method
摘要 A submarine launched missile generates undesirable stress on the rocket nozzle hydraulic control system at the moment of ignition of the rocket motor. This stress can be minimized by operating the system so that the nozzle is near center and the hydraulic actuator valves are open at ignition.
申请公布号 US5115710(A) 申请公布日期 1992.05.26
申请号 US19910674275 申请日期 1991.02.19
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY 发明人 MITCHELL, DAVID L.;STEIN, ALAN J.;BARNDT, JR., CHARLES L.;SZETO, WILLIAM W.
分类号 F02K9/84;F42B15/20 主分类号 F02K9/84
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