FIELD: transport.
SUBSTANCE: invention relates to transport spacecraft (TSC) flights between two orbital stations (OS), one of which is located on atmosphere planet orbit, and another one is either on other celestial body orbit (for example, the Moon) or near libration points (for example, L1 or L2 of Earth-Moon system). Proposed method comprises TSC undocking from circumplanetary OS, its bringing on boosters (BM) module support orbit, TSC approach and docking to BM module. Then to formed packet pulses for flight to remote OS are applied. For return travel to TSC reverse pulse is applied and then, several series of flights in planet atmosphere are performed for TSC deceleration to circular on circumplanetary OS orbit. After that, TSC is docked to OS.
EFFECT: technical result is possibility to create over a short period of time and at low costs on its development of transportation system between Earth OS and remote OS.
1 cl, 4 dwg
