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Engine Model: 15D151. Government Designation: 15D151. Designer: NII-125. Developed in: 1964-69. Application: Combined missile (RT-20P) stage 1. Gross Mass: 19,150 kg (42,210 lb). Empty Mass: 2,450 kg (5,400 lb). Propellants: Solid. Thrust(sl): 588.000 kN (132,187 lbf). Burn time: 65 sec. Diameter: 1.60 m (5.20 ft). Length: 6.12 m (20.07 ft). Chambers: 4. Country: Ukraine. Status: Out of production. First Flight: 1967. Last Flight: 1969. Flown: 12.

Designed for first stage of combined missile and SLBM; flight tested, no production.

15D151 used on Rocket Stages
Bibliography:

  • Pervov, Mikhail, Raketnoye Oruzhiye RVSN, Violanta, Moscow, 1999..
  • Karpenko, A V, Utkin, A F and Popov,A D, Otechestvenniye strategischeskiye raketnoye kompleks, Sankt-Peterburg: Nevskii bastion; Gangut 1999..
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