The purpose of the present invention is to provide a low-cost rocket which can be reused at low cost. The low-cost rocket is composed of an in-atmosphere flight part and an out-atmosphere flight part, and in the atmosphere, the in-atmosphere flight part ascends through air, so that the in-atmosphere flight part and the out-atmosphere flight part are separated near the outside of the atmosphere. The flight part outside the atmospheric layer ascends to the outside of the atmospheric layer through the rocket, and the flight part inside the atmospheric layer descends and lands by utilizing air.
本发明的目的在于提供一种以低成本实现能够再使用的火箭的低成本火箭。所述低成本火箭由大气层内飞行部分和大气层外飞行部分构成,在大气层内通过所述大气层内飞行部分利用空气上升,使所述大气层内飞行部分与所述大气层外飞行部分在大气层外附近分离,所述大气层外飞行部分通过该火箭上升到大气层外,所述大气层内飞行部分利用空气下降并着陆。
Low-cost rocket
低成本火箭
2021-10-01
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
Rocket Propulsion Cost Modeling
Springer Verlag | 1989
|Cost reduction criteria (rocket engines)
AIAA | 1969
|