To solve the problem that, while the following methods [1] chemical rockets, [2] electrical rockets, and [3] swing-by are conventionally available for obtaining propulsion power in transition flights (interplanetary flights) of a planetary probe in the aero-space, these methods have advantages and drawbacks with regard to "magnitude of thrust" and "acceleration possible time" and the like, and therefore there is a need for a propulsion method that more efficiently enables long distance flights.SOLUTION: A cylindrical hollow device is loaded with gunpowder and a matter (solid) using a mechanism different from that of a conventional propulsion device. When the gunpowder in the cylinder is exploded, the matter (solid) is fired (ejected) outside of the cylinder. Provided is a device (rocket) that utilizes a counterreaction (reaction) of the firing (ejection) action of the matter (solid) obtained at this time, as propulsion power.SELECTED DRAWING: None
【課題】従来、惑星探査機の宇宙空間における遷移飛行(惑星間の飛行)において、推進力を得るための方法として、次のようなものがある。▲1▼化学ロケット、▲2▼電気ロケット、▲3▼スイングバイこれらの方法は、「推力の大きさ」、「加速可能時間」等で一長一短があり、より効率的に長距離飛行可能な推進方法が求められていた。【解決手段】従来の推進装置とは異なる仕組みで、筒型中空の装置内に火薬と物体(固体)を装填する。この筒型内の火薬を爆発させることで、物体(固体)を筒型外へ発射(放出)する。この時得られる物体(固体)の発射(放出)作用の反作用(反動)を利用して推進力とする装置(ロケット)を提供し、課題を解決する。【選択図】なし
EXPLOSIVE ROCKET
火薬ロケット
2023-03-01
Patent
Electronic Resource
Japanese
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