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|family = R-7 |status = Retired |sites = Baikonur Site 31/6 |launches = 3 |success = 3 |first = 24 November 1970 |last = 12 August 1971 |payloads = LK |stagedata = }} The Soyuz-L ((ロシア語:Союз), meaning "union"), GRAU index 11A511L was a Soviet expendable carrier rocket designed by OKB-1 and manufactured by State Aviation Plant No. 1 in Samara, Russia. It was used for tests of the LK Lunar lander in low Earth orbit, as part of the Soviet lunar programme. The Soyuz-L was essentially a two-stage derivative of the Molniya-M, itself derived from the original Soyuz. It featured the reinforced first stage and boosters used to provide support for the Molniya's third stage, allowing it to carry a larger and more massive payload. A larger payload fairing was also fitted, to accommodate the LK spacecraft. The Soyuz-L made its maiden flight in 1970, and was retired in 1971, having made three launches. All three launches were successful.〔 The later Soyuz-U used a similar configuration to the Soyuz-L. ==References== 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「Soyuz-L」の詳細全文を読む スポンサード リンク
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