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RT-2M


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z RT-2M Part of RT-2 Russian intercontinental ballistic missile. The RT-2M was a modernized RT-2, developed under Savodskiy at Korolev's bureau beginning in the late 1960's in parallel with the RT-2P and using alternate new engines. This increased both range and payload compared to the RT-20. However the RT-2P was selected for further development.

AKA: 8K98M. Payload: 800 kg (1,760 lb). Gross mass: 50,000 kg (110,000 lb). Height: 21.13 m (69.32 ft). Diameter: 1.84 m (6.03 ft). Span: 3.62 m (11.87 ft). Apogee: 1,000 km (600 mi).

The RT-2M was a modernized RT-2, developed under Savodskiy at Korolev's bureau beginning in the late 1960's in parallel with the RT-2P and using alternate new engines. This increased both range and payload compared to the RT-20. However the RT-2P was selected for further development.

Maximum range: 10,000 km (6,000 mi). Number Standard Warheads: 1. Warhead yield: 900 KT. CEP: 1.80 km (1.10 mi). Boost Propulsion: Solid.

Family: ICBM. Country: Russia. Launch Sites: Plesetsk. Stages: 15D23P, 15D94, 15D27. Agency: Korolev bureau. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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