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A-105 (SA-10) : ウィキペディア英語版 | AS-105 (spacecraft)
AS-105 was the fifth and final orbital flight of a boilerplate Apollo spacecraft, and the third and final launch of a Pegasus micrometeroid detection satellite. It was launched by SA-10, the tenth and final Saturn I carrier rocket,in 1965. == Overview == AS-105 was an Apollo boilerplate spacecraft; boilerplate BP-9A was used for the flight. The spacecraft reentered on November 22, 1975.〔(【引用サイトリンク】 title=Saturn I )〕 The Saturn launch vehicle (SA-10) was similar to those of missions AS-103 and AS-104. As on the previous mission, the boilerplate service module was equipped with a test installation of a reaction control engine package. The primary flight objective was to continue demonstration of the launch vehicle's iterative guidance mode and evaluation of system accuracy.
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「AS-105 (spacecraft)」の詳細全文を読む
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