发明名称 CONTROLLER FOR IGNITION OF ROCKET
摘要 PURPOSE:To simplify the interface between the rocket and the ground by providing a timer loading the rocket controlled from the ground while providing a command receiver operated by instructions from a ground station. CONSTITUTION:A rocket is provided with a timer 6 controlled from the ground and the command receiver 12. A safety switch 2 and a motor switch 3 are turned ON by an operation power supply 12, the power supply is applied to an ignition system 5 by signals from the timer 6, and a first stage of the rocket is ignited. When the safety switch 2, the motor switch 3 and the timer device 6 cannot be stopped for some reason, a drive circuit 13 is actuated through instructions to the command receiver 12 by radio by a command transmitter 14, and each switch 2, 3 and the timer 6 can be stopped. Accordingly, the interface between the rocket and the ground can be simplified, and safety can also be ensured sufficiently.
申请公布号 JPS58158355(A) 申请公布日期 1983.09.20
申请号 JP19820042054 申请日期 1982.03.16
申请人 MATSUSHITA DENKI SANGYO KK 发明人 SEKI TOSHIO
分类号 B64G1/24;F02K9/95;(IPC1-7):02K9/95 主分类号 B64G1/24
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