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RT-25
Russian intermediate range ballistic missile. Decree 316-157 of 4 April 1961 authorized development of a family of solid propellant launch vehicles utilizing various combinations of three stages (the RT-2, RT-15, and RT-25). The RT-25 IRBM used the first and third stages of the RT-2 ICBM. M Yu Tsirulnikov at SKB-172 in Perm was responsible for development of the RT-25. However there was little interest in this variant and in 1963 further development was dropped.

AKA: 8K97. Status: Cancelled 1963. Thrust: 892.00 kN (200,529 lbf). Gross mass: 41,000 kg (90,000 lb). Height: 16.00 m (52.00 ft). Diameter: 1.84 m (6.03 ft). Span: 2.00 m (6.50 ft).

Maximum range: 4,500 km (2,700 mi).



Family: IRBM. Country: Russia. Agency: Tsirulnikov bureau. Bibliography: 475, 476, 8557.

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