发明名称 Rocket solid propellant charge - is partially housed in case with ignition and priming
摘要 <p>The shell or rocket has a case (2) with a nose cap (1). The case is fitted in the rear with a war head (3). The charge is ignited by the ignitor (4) behind the grill (5). Priming is effected by a cap (6) located in the tube (7) and protected by the shield (8). The propellant block (9) is housed in the case (2) and has a central passage (11). The outside surface of the block is inhibited and the top end remains uncovered over a length (E).</p>
申请公布号 FR2479905(A1) 申请公布日期 1981.10.09
申请号 FR19800007517 申请日期 1980.04.03
申请人 ETAT FRANCAIS 发明人 ANDRE JEAN, MICHEL COISPLET ET ALAIN CHEVALIER
分类号 F02K9/10;F02K9/26;(IPC1-7):02K9/10;42B15/00;42B13/00 主分类号 F02K9/10
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