To provide a launch system, a launch vehicle and a method of launching a payload for delivery of the payload at a terrestrial location, an Earth orbital location, or an extraorbital location.SOLUTION: A launch vehicle 200 of the present invention comprises a payload 240, a propellant tank 230, an electrical heater 220 in which propellant, such as light gas (e.g., hydrogen) is electrically heated, and an exhaust nozzle 210 from which the heated propellant expands to provide an exhaust velocity of, for example, 7-16 km/sec. The launch vehicle 200 is utilized with the launch system, which further comprises a launch tube 100 formed of at least a tube 110 and a tube 130, which are electrically conductive and which are combined with at least one insulator tube 120. An electrical energy source is also provided.SELECTED DRAWING: Figure 1
【課題】地球の場所、地球軌道の位置または軌道外の位置に、ペイロードを送達できる発射システム、発射輸送手段およびペイロード発射方法を提供する。【解決手段】発射輸送手段200は、ペイロード240、推進剤タンク230、軽ガス(例えば水素)のような推進剤が電気的に加熱される電気加熱器220、および、そこから加熱された推進剤が膨張し、例えば7〜16km/秒の排出速度をもたらす排出ノズル210を備える。発射輸送手段200は発射システムと共に使用可能であり、発射システムは少なくともチューブ110、チューブ130で形成された発射チューブ100をさらに有する。それらは導電性であり、少なくとも1つの絶縁体チューブ120と組み合わせる。電気エネルギー源もまた提供可能である。【選択図】図1
LAUNCH VEHICLE AND SYSTEM AND METHOD FOR ECONOMICAL AND EFFICIENT LAUNCH THEREOF
発射輸送手段およびシステムおよびその経済的、効率的発射方法
2019-02-28
Patent
Elektronische Ressource
Japanisch
IPC: | F41F APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS , Vorrichtungen zum Abschießen von Geschossen oder Flugkörpern aus Rohren, z.B. Geschütze / B64G Raumfahrt , COSMONAUTICS / F03H PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR , Erzeugung von Vortriebskraft [Schub] nach dem Prinzip des Rückstoßes, soweit nicht anderweitig vorgesehen / F41B WEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE , Waffen zum Verschießen von Geschossen ohne Verwendung von Explosiv- oder Treibladungen |
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