[problem] less likely to be affected is the initial speed at a high speed of weather immediately after withdrawal from the launch pad, providing a launch pad of very little rocket fuel consumption of propellant. Entrance derived accessory functions necessary for A container (cylinder) of a single cylindrical side is closed of the two ends in the structure is 12 to high speed increase straight running of a rocket of the instrument and the acceleration purpose of propulsion equipment (piston) 10 and the possession of the exhaust gas or waste generated after the explosion of the internal combustion chamber 18, 20, the two places have explosives other than propellant inside the rocket as an internal combustion engine to the outside is housed in a sealed state in the cylinder 12 within features a structure that does not leak or scatteringFIELD 8
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