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Earth orbit rendezvous : ウィキペディア英語版 | Earth orbit rendezvous
Earth orbit rendezvous (EOR) is a potential methodology for conducting round trip human flights to the Moon, involving the use of space rendezvous to assemble, and possibly fuel, components of a translunar vehicle in low Earth orbit.〔"LOW EARTH ORBIT RENDEZVOUS STRATEGY FOR LUNAR MISSIONS" http://www.informs-sim.org/wsc06papers/158.pdf〕 It was considered and ultimately rejected in favor of lunar orbit rendezvous (LOR) for NASA's Apollo Program of the 1960s and 1970s.〔"Lunar Orbit Rendezvous and the Apollo Program" http://www.nasa.gov/centers/langley/news/factsheets/Rendezvous.html〕 Three decades later, it was planned to be used for Project Constellation, until that program’s cancellation in October 2010.〔Connolly, John F. (October 2006). "Constellation Program Overview" http://www.nasa.gov/pdf/163092main_constellation_program_overview.pdf〕 ==Gemini and Agena target vehicle== The Agena target vehicle was used for testing Earth orbit rendezvous in the NASA Gemini Program. Gemini 6 and Gemini 7 rendezvoused in orbit in 1965, but without Agena. Next, Gemini 8 successfully docked March 16, 1966 with the Agena. The Agena-Gemini rendezvous also achieved many other tasks in later Gemini launches.
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Earth orbit rendezvous」の詳細全文を読む
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