Russian intercontinental range ballistic missile. Variant using a Glushko nuclear engine heating ammonia as a propellant.
Payload: 4,000 kg (8,800 lb) to a 14,000 km range.
Gross mass: 84,400 kg (186,000 lb).
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Payload: 4,000 kg (8,800 lb).
Height: 25.00 m (82.00 ft).
Diameter: 3.33 m (10.92 ft).
Thrust: 1,260.00 kN (283,250 lbf).
YaRD OKB-456 Glushko nuclear/ammonia rocket engine. 1373 kN. Development ended 1960. Isp=470s. Used nuclear reactor in cylindrical housing, operating at 3000 deg K. Propellant heated in the reactor and exhausted through four expansion nozzles More...
YaRD ICBM Single-stage nuclear-powered ICBM designed by OKB-1.
A 30 June 1958 resolution authorised development of this astounding weapon, and the draft project was completed on 30 December 1959. Perhaps coming under the heading of 'inadvisable rocket science', test launches would have been into an artificial reservoir in the target area to limit contamination by having the reactor crash into water at the end of its trajectory. More...
missile Guided self-propelled military weapon (as opposed to rocket, an unguided self-propelled weapon). More...
Associated Manufacturers and Agencies
Korolev Russian manufacturer of rockets, spacecraft, and rocket engines. Korolev Design Bureau, Kaliningrad, Russia. More...
YaRD ICBM OKB-456 Nuclear/Ammonia propellant rocket stage. Loaded/empty mass 84,400/8,600 kg. Thrust 1,370.00 kN. Vacuum specific impulse 470 seconds. Nuclear-propelled ICBM with engines in development by Glushko. Four expansion nozzles fed by single reactor. Payload 2,600 kg to 14,000 km. Empty mass, vehicle length calculated. More...
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