Zobrazeno 1 - 10
of 109
pro vyhledávání: '"Earth orbit rendezvous"'
Publikováno v:
Journal of Spacecraft and Rockets. 57:767-776
Although the historical and technical details of Project Apollo have been extensively documented in literature, current records indicate that there is still a lack of an early-design-phase, physics...
Publikováno v:
Advances in Space Research. 60:2505-2517
In this paper a rendezvous mission to the Earth’s Trojan asteroid 2010 TK 7 is proposed, and preliminary transfer trajectories are designed. Due to the high inclination ( ∼ 20.9°) of the target asteroid relative to the ecliptic plane, direct tra
Publikováno v:
Journal of Guidance, Control, and Dynamics. 39:2170-2178
Publikováno v:
Advances in Space Research
Advances in Space Research, Elsevier, 2016, 57 (11), pp.2376-2384. ⟨10.1016/j.asr.2016.03.007⟩
Advances in Space Research, Elsevier, 2016, 57 (11), pp.2376-2384. ⟨10.1016/j.asr.2016.03.007⟩
International audience; The Chang'E-5 mission is the third phase of the Chinese Lunar Exploration Program and will collect and return lunar samples. After sampling, the Orbiter and the ascent vehicle will rendezvous and dock, and both spacecraft will
Autor:
R. F. Murtazin
Publikováno v:
Cosmic Research. 54:253-259
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 la
Publikováno v:
Journal of Guidance, Control, and Dynamics. 38:315-322
AUTONOMOUS lunar rendezvous missions have drawn increasing interest in recent years due to the future human and robotic lunar exploration applications [1,2]. For example, the Chinese lunar exploration mission phase III, scheduled for launch in 2017,
Akademický článek
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Publikováno v:
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Publikováno v:
Acta Mechanica Sinica. 30:966-972
Asteroid exploration trajectories which start from a lunar orbit are investigated in this work. It is assumed that the probe departs from lunar orbit and returns to the vicinity of Earth, then escapes from the Earth by performing a perigee maneuver.
Autor:
Rafail Murtazin
Publikováno v:
Acta Astronautica. 101:151-156
There was a lot of experience gained in the rendezvous of different vehicles in the LEO during the years of human space exploration. In the framework of the Apollo program when the astronauts landed on the surface of the Moon, the docking of the Luna