UR-100NU 15A35S (original) (raw)
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UR-100NU 15A35S
Russian intercontinental ballistic missile.
Status: Retired 1986. First Launch: 1982-10-21. Last Launch: 1986-01-01. Number: 11 . Gross mass: 105,600 kg (232,800 lb). Height: 24.30 m (79.70 ft). Diameter: 2.50 m (8.20 ft). Apogee: 1,000 km (600 mi).
Maximum range: 10,000 km (6,000 mi).
Family: ICBM. Country: Russia. Launch Sites: Baikonur. Stages: UR-100N Stage 1N, UR-100N Stage 2N, UR-100N MIRV Bus. Agency: Chelomei bureau.
1982 October 21 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35S.
- SLI - . Nation: Kazakhstan. Agency: RVSN. Apogee: 0 km (0 mi).
1982 December 8 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35S.
- SLI - . Nation: Kazakhstan. Agency: RVSN. Apogee: 0 km (0 mi).
1982 December 22 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35S. FAILURE: Failure.
1983 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35S.
1983 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35S.
1983 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35S.
1983 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35S.
1983 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35S.
1983 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35S.
1984 December 6 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35S. FAILURE: Failure.
1986 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35S.
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