Multiple pulse cartridge ignition system专利检索- .使用增加推进力的接连装置的极高速导弹推进器例如使用沿身管全长安排的连续起爆推进装药;多级火箭推进器专利检索查询-专利查询网

Multiple pulse cartridge ignition system
申请号	EP01102856.0	申请日	2001-02-13	公开(公告)号	EP1126233A3	公开(公告)日	2002-03-27
申请人	ALLIANT TECHSYSTEMS INC.;			发明人	Crickenberger, Andrew B.; Ghazi, Saleem L.;
摘要	An electronically controlled multi-pulse ignitor ignites a cartridge used to launch a projectile (50). An electronics module (9) is programmed with a temperature performance profile for the cartridge. A temperature sensor is coupled to supply current cartridge temperature data to the electronics module (9). A first event ignitor is coupled to the electronics module (9) and initiates a ballistic cycle upon command from the electronics module (9). A translation mechanism (64), including a first charge coupled to the first event ignitor, moves the projectile (50) forward to increase the free volume in the cartridge. A second event ignitor (70), coupled to receive a second event ignition signal from the electronics module (9), ignites the main propellant charge on receiving the second event ignition signal from the electronics module (9), where the timing of ignition of the second event ignitor (70) is determined by the temperature performance profile and the current cartridge temperature data.
权利要求
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