发明名称 ROCKET MOUNTED SUB WARHEAD EJECTING DEVICE
摘要 PROBLEM TO BE SOLVED: To eject sub warheads with time difference and speed difference while reducing ejecting cost, improving assembly workability, and securing high reliability. SOLUTION: The rocket mounted sub warhead ejecting device is provided with a plurality of combustion chambers 2 communicated with at least one sub warhead housing container C positioned on a circumference of a rocket R and housing sub warheads B so they can be released in centrifugal directions, and sub warhead ejecting explosives 3 respectively arranged in the combustion chambers 2. An igniter 4 is connected to the warhead ejecting explosive 3A for a first state combustion chamber 2A of the plurality of combustion chambers 2. Ignition mechanisms 10 receiving combustion gas G caused by combustion of the sub warhead ejecting explosives 3A and 3B in the combustion chambers 2A and 2B, sequentially operating, and igniting each sub warhead ejecting explosives 3B and 3C are respectively provided in the combustion chambers 2B and 2C of a second stage and onward subsequent to the first stage combustion chamber 2A. COPYRIGHT: (C)2004,JPO
申请公布号 JP2004044884(A) 申请公布日期 2004.02.12
申请号 JP20020202064 申请日期 2002.07.11
申请人 IHI AEROSPACE CO LTD 发明人 ISHIKAWA TOMOTAKA;MORI MAMORU
分类号 F42B12/60;(IPC1-7):F42B12/60 主分类号 F42B12/60
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