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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).
1971 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1971 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1971 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1971 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1971 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1971 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1971 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1971 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1971 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1971 February 2 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- First State trials launch - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1971 February 12 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1971 September 1 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- Operational test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1984 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- Operational test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1984 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- Operational test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1984 - .
Launch Site:
Baikonur.
LV Family:
UR-100.
Launch Vehicle:
UR-100M.
- Operational test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
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