发明名称 PRECISION GUIDANCE SYSTEM FOR AIRCRAFT LAUNCHED BOMBS
摘要 A jet bomb guidance system in which bi-directional nozzles are fired in a manner to produce force state changes resulting in improved level of control, greater force compatibility and greater efficiency in propellant fuel usage The system includes four bi-directional nozzles spaced at 90 degree intervals which at least four single nozzles are open at any given instant to maintain a substantially constant gas pressure. The system may be positioned at the nose portion, tail portion, or center of gravity of the bomb.
申请公布号 US2002153448(A1) 申请公布日期 2002.10.24
申请号 US20010862843 申请日期 2001.05.23
申请人 MAYERSAK JOSEPH R. 发明人 MAYERSAK JOSEPH R.
分类号 F41G7/00;F41G7/34;F42C19/00;(IPC1-7):F42B15/01;F42B10/00 主分类号 F41G7/00
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