发明名称 A BOMB FOR DEPLOYMENT FROM AN AIR VEHICLE
摘要 <p>A bomb for deployment from an air vehicle includes a rocket motor (1) for propelling the bomb. The rocket motor includes propellant (5) which at least partially defines a void (11) downstream of an initial burning surface. As the propellant (5) is burned the void 11 will be exposed, increasing the surface area of the burning surface (9) of the propellant (5) to increase the thrust of the rocket motor.</p>
申请公布号 WO2013001267(A1) 申请公布日期 2013.01.03
申请号 WO2012GB00552 申请日期 2012.06.28
申请人 MBDA UK LIMITED;IRVINE, RODNEY, ANDREW 发明人 IRVINE, RODNEY, ANDREW
分类号 F02K9/18;F02K9/22;F42B15/10 主分类号 F02K9/18
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