To solve the problem of methods used in which artificial satellites and planetary probes in prior art are loaded on rockets to be launched and put in satellite orbits, or directed to target planets by utilizing gravity of the earth, or the like.SOLUTION: In order to solve the problem, an electric propulsion function is loaded into an artificial satellite or a planetary probe. A slit (notch) is formed in one piece of disk type plate, and the plate is rotated at high speed to cause fluid movement so that conversion to propulsive power occurs. A bullet is fired from a gun barrel installed in an airframe, whereby conversion to propulsive power occurs utilizing a reaction (counteraction) at this time. A wall is installed on an outer peripheral lateral surface of the airframe, so that fluid resistance is reduced and high-speed movement is facilitated.SELECTED DRAWING: None
【課題】従来の人工衛星や惑星探査機は、ロケットに搭載して打ち上げて衛星軌道に乗せる、地球の重力を利用して目標惑星へ向かわせるなどの方法が使用されていた。【解決手段】人工衛星、惑星探査機に電動の推進機能を搭載し、課題を解決する。円盤型1枚板にスリット(切れ込み)を入れ、高速回転することで流体移動を起こし、推進力に変換する。機体に設置した砲身から弾丸を発射して、この時の反動(反作用)を利用して推進力に変換する。機体外周側面に壁を設置し、流体抵抗を低減し高速移動しやすくする。【選択図】なし
ELECTRIC PROPULSION TYPE ARTIFICIAL SATELLITE AND PLANETARY PROBE
電動推進式人工衛星、及び惑星探査機
2024-01-09
Patent
Electronic Resource
Japanese
IPC: | B64G Raumfahrt , COSMONAUTICS |