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RD-108-11D512P
Part of RD-107
RD-107
RD-107
Credit: © Mark Wade
Glushko LOx/Kerosene rocket engine. Soyuz 11A511U2-1. Out of production. A 1-2 second specific impulse increase was made possible by the use of synthetic fuel Sintin and a modified mixing head. First flight 1982.

AKA: 11D512P. Status: Out of production. Number: 92 . Thrust: 1,011.00 kN (227,281 lbf). Specific impulse: 319 s. Specific impulse sea level: 252 s. Burn time: 290 s.

This was a very complicated modification. Diameter is per chamber.

Chambers: 4. Thrust (sl): 788.400 kN (177,239 lbf). Thrust (sl): 80,400 kgf.

Country: Russia. Launch Vehicles: Soyuz-U2. Propellants: Lox/Kerosene. Stages: Soyuz 11A511U2-1. Agency: Glushko bureau.
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