发明名称 Missile launch safety enhancement apparatus
摘要 <p>A missile launch safety enhancement apparatus (135) for inhibiting the launch sequence of a missile launched from an aircraft-based or land vehicle-based missile launch system. The apparatus (135) incorporates means for producing a prefire signal (102a). The prefire signal produced is then compared to a reference signal level by comparing means (167). If the prefire signal is not below the reference signal level by a predetermined amount, interrupting means (216, 240) inhibits the firing sequence of the missile and thus prevents the missile from being launched. If the prefire signal is below the reference signal level by a predetermined amount indicating proper current drawn by the circuit, the firing sequence is not inhibited, and the missile is launched. &lt;IMAGE&gt;</p>
申请公布号 EP0713074(A1) 申请公布日期 1996.05.22
申请号 EP19950308113 申请日期 1995.11.14
申请人 HUGHES AIRCRAFT COMPANY 发明人 WELLS, MICHAEL L.
分类号 F41F3/055;F41F3/06;F41G7/00;(IPC1-7):F41G7/00 主分类号 F41F3/055
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