UR-100M (original) (raw)

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UR-100M

Part of UR-100

Russian intercontinental ballistic missile. The 8K84M was an improved version of the UR-100 with an improved empty mass fraction, a new guidance system, countermeasures capability, and post-boost maneuverability to defeat enemy anti-ballistic missile systems.

AKA: 15P084;8K84M;8K84UTTKh;RS-10;Sego;SS-11 Mod.2. Status: Retired 1984. First Launch: 1970-01-01. Last Launch: 1984-01-01. Number: 27 . Payload: 1,050 kg (2,310 lb). Thrust: 876.00 kN (196,932 lbf). Gross mass: 50,100 kg (110,400 lb). Height: 18.90 m (62.00 ft). Diameter: 2.00 m (6.50 ft). Span: 2.00 m (6.50 ft). Apogee: 1,000 km (600 mi).

Development was authorized on 9 December 1965. Twelve trial flights were conducted between 23 July 1969 and 15 March 1971. The system was formally accepted by the military on 3 October 1972. The first regiment became operational at Khmelnitskiy on 1 March 1970.

Tests were made with a radar system to provide improved accuracy with a one megaton warhead at 9200 km range, but this was not adopted for service. Although this missile is often referred to as the UR-100M, this designation was applied within the design bureau to a naval version of the UR-100 developed by Chelomei in 1962-1964, but not selected for full development or production.

Maximum range: 13,000 km (8,000 mi). Number Standard Warheads: 1. Warhead yield: 1,200 KT. CEP: 1.10 km (0.60 mi). Boost Propulsion: Storable liquid rocket, N2O4/UDMH. Cruise engine: 8D423. Initial Operational Capability: 1970. Total Number Built: 590.

Family: ICBM. Country: Russia. Engines: RD-0216. Launch Sites: Baikonur. Stages: 8S816, 8S817. Agency: Chelomei bureau.

1970 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 July 27 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 July 28 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 August 1 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 August 1 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100M.

Operational missile test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).