发明名称 Control after burnout for reaction steered missiles
摘要 The warhead of a missile is loaded with a payload that can either be burned or exploded. If propulsion is lost and either aerodynamic steering is not present or the velocity level of the missile is degraded to a point where steering is marginal, steerage is maintained by igniting the warhead payload and exhausting gases through nozzles attached to the warhead.
申请公布号 US4078495(A) 申请公布日期 1978.03.14
申请号 US19740499233 申请日期 1974.08.15
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY 发明人 LEDDEN, JR., WILLIAM J.
分类号 (IPC1-7):F42B13/30 主分类号 (IPC1-7):F42B13/30
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