Tsiklon-2A

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概览

Tsiklon-2A是乌克兰Yuzhnoye Design Bureau研制的运载火箭(已退役/停用)。全长 39.7 米、直径 3 米、起飞质量 182 吨、近地轨道运力 3 吨。1967-10-27 首飞,迄今发射 8 次、成功 7 次。

状态退役/停用
制造方Yuzhnoye Design Bureau (OKB-586)
国家 / 地区乌克兰
级数2
全长40 m
直径3 m
起飞质量182 t
LEO 运力3,000 kg
GTO 运力
起飞推力2,366 kN
首飞1967-10-27
发射战绩成功 7 / 共 8

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英文简介

The Tsyklon was a Soviet-designed expendable launch system, primarily used to put Cosmos satellites into low Earth orbit. It is based on the R-36 intercontinental ballistic missile designed by Mikhail Yangel and made eight launches, with seven successes and one failure. All of its launches were conducted from LC-90 at the Baikonur Cosmodrome. It is sometimes designated Tsyklon-2A, not to be confused with the later Tsyklon-2 rocket. It was introduced in 1967 and was derived from the R-36 ICBM (NATO designation SS-9 Scarp). It was retired in 1969.

快速问答

Tsiklon-2A目前是否现役?
否,数据库当前标记为退役或停用。
Tsiklon-2A由谁制造?
制造方为 Yuzhnoye Design Bureau。
Tsiklon-2A的近地轨道运力是多少?
当前收录的 LEO 运力为 3,000 kg。

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