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公开(公告)号:US4023354A
公开(公告)日:1977-05-17
申请号:US200247
申请日:1971-11-18
申请人: Ronald F. Vetter , James P. Diebold , George F. Sieg , Howard W. Gerrish, Jr. , Howard H. Payne , Elmer J. Rhyn , Irvin F. Witcosky
发明人: Ronald F. Vetter , James P. Diebold , George F. Sieg , Howard W. Gerrish, Jr. , Howard H. Payne , Elmer J. Rhyn , Irvin F. Witcosky
摘要: Slurried rocket propellants and a spinning rocket motor wherein the propents have viscosities which enable them to form central cores when spun in spinning rocket motors, the motor having a diaphragm-like base plate which assists in transferring forward momentum through the propellant.
摘要翻译: 制浆火箭推进剂和旋转火箭发动机,其中推进剂具有粘度,使得它们能够在纺丝火箭发动机中旋转时形成中心芯,该电动机具有有助于将推进动力传递通过推进剂的隔膜状基板。