Sсheme of rendezvous mission to lunar orbital station by spacecraft launched from Earth
| Autor: | R. F. Murtazin |
|---|---|
| Rok vydání: | 2016 |
| Předmět: |
Engineering
010504 meteorology & atmospheric sciences Spacecraft business.industry Astrophysics::Instrumentation and Methods for Astrophysics Rendezvous Aerospace Engineering Astronomy and Astrophysics Lunar orbit Moon landing 01 natural sciences Physics::Geophysics Astrobiology Service module Space and Planetary Science Physics::Space Physics 0103 physical sciences Astrophysics::Earth and Planetary Astrophysics Earth orbit rendezvous Aerospace engineering Orbital maneuver business 010303 astronomy & astrophysics 0105 earth and related environmental sciences Space rendezvous |
| Zdroj: | Cosmic Research. 54:253-259 |
| ISSN: | 1608-3075 0010-9525 |
| DOI: | 10.1134/s0010952516030059 |
| Popis: | In recent years, great experience has been accumulated in manned flight astronautics for rendezvous in near-Earth orbit. During flights of Apollo spacecraft with crews that landed on the surface of the Moon, the problem of docking a landing module launched from the Moon’s surface with the Apollo spacecraft’s command module in a circumlunar orbit was successfully solved. A return to the Moon declared by leading space agencies requires a scheme for rendezvous of a spacecraft launched from an earth-based cosmodromee with a lunar orbital station. This paper considers some ballistic schemes making it possible to solve this problem with minimum fuel expenditures. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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