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 |
同系列火箭型号
按上游火箭家族字段关联,便于比较不同构型。
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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