P-100
P-100
Credit - © Mark Wade
Intercontinental cruise missile. Year: 1961. Family: Soviet Strategic Cruise Missiles. Country: Russia.

Family of sea- or silo- launched Mach 3.5 cruise missiles with ranges up to intercontinental distances.

The P-100 was Beriev's entry in the long-range cruise missile competition at the beginning of the 1960's. Work on the draft project began in 1961. The concept was a single ramjet-powered missile that could be adapted for launch from fixed silos, aircraft, surface ships, and submarines. The project had a scheduled completion of 1965 but was cancelled at the study stage.

Variants considered included:

  • Attack version for launch by the specially designed UDD (long range strike boat) design of TsKB-17 or hardened (40 kgf/sq cm) silos. 14 tonne mass, with launch by 4 solid motors, each 8 m long x 0.8 to 1.0 m in diameter. Range 150 to 2000 km, cruise at 25 to 30 km altitude at 3500-4000 km/hr. Length 11.4 m, diameter 1.24 m, wingspan 2.3 m.
  • Reconnaisance version for launch from UDD strike boat or hardened silos. 20 tonne mass, with launch by 4 solid motors. Range 2500 km, cruise at 25 to 30 km altitude at 3500-4000 km/hr. Length 12.0 m, diameter 1.3 m, wingspan 3.4 m.
  • Silo-launched intercontinental cruise missile variant. This would use a huge booster stage, similar to the German A9/A10 concept. The thermonuclear warhead would be delivered using inertial/stellar guidance by NII-17 GKRE. and the missile would achieve 6000 km range, cruising at 25 to 50 km at 3500-4000 km/hr. The booster would have been 20 m long, 2.5 m in diameter, with a total mass of 40 tonnes. The cruise stage would have been a 20 tonne version of the basic missile.

Manufacturer: Beriev. Total Mass: 60,000 kg (132,000 lb). Core Diameter: 2.50 m (8.20 ft). Total Length: 32.00 m (104.00 ft). Span: 2.50 m (8.20 ft). Maximum range: 6,000 km (3,700 mi). Number Standard Warheads: 1. Boost Propulsion: Storable liquid rocket. Cruise Propulsion: Ramjet. Guidance: Inertial/stellar. Maximum speed: 4,000 kph (2,400 mph). Ceiling: 30,000 m (98,000 ft).



Bibliography and Further Reading
  • Pervov, Mikhail, Raketnoye Oruzhiye RVSN, Violanta, Moscow, 1999.. Narrative overview of the missiles of the Russian strategic missile forces.
  • Karpenko, A V, Utkin, A F and Popov,A D, Otechestvenniye strategischeskiye raketnoye kompleks, Sankt-Peterburg: Nevskii bastion; Gangut 1999.. Well-illustrated encyclopedia of the missiles of the Russian strategic missile forces.
 
 
 
 
 
 
 
 
 

Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2007 except where otherwise noted.

 
Encyclopedia Astronautica
topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z