POWER SOURCE DEVICE FOR IGNITION

PROBLEM TO BE SOLVED: To provide a power source device for ignition capable of contributing to the mobility of a launching device and quickly and adequately performing preparation for launch even in an emergency situation. SOLUTION: A rocket 1 is provided with a propulsion unit 10 inside, and the pr...

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Bibliographische Detailangaben
1. Verfasser:	MURAHASHI TOSHIAKI
Format:	Patent
Sprache:	eng
Schlagworte:	AMMUNITION APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS BASIC ELECTRIC ELEMENTS BLASTING ELECTRICITY EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HARPOON GUNS HEATING LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MECHANICAL ENGINEERING PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a power source device for ignition capable of contributing to the mobility of a launching device and quickly and adequately performing preparation for launch even in an emergency situation. SOLUTION: A rocket 1 is provided with a propulsion unit 10 inside, and the propulsion unit 10 incorporates a propellant. One end of the propulsion device 10 is provided with an ignition circuit 11, and the other end is connected to a nozzle 12 mounted at the rear end of the rocket 1. A launch control device 2 comprises a launch control circuit 20 and a power source device 21 for ignition. The launch control circuit 20 is electrically connected to the ignition circuit 11, and controls the supply of a DC to the ignition circuit 11 on the basis of an electromotive force generated in the power source device 21 for ignition. COPYRIGHT: (C)2007,JPO&INPIT