R95-300 (RDK-300) / RD95TM-300
- dual-stream engine used in Ch-35, Ch-55, Ch-55SM, Ch-555, RK-55 Relief missiles, S-10 Grenade, Ch-59, Ch-101, Ch-102, Biryuza / Kalibr (Club)
- RDK-300 trade name for R95-300 (in orig. RDK-300 - Jet Engine Kommerческий, 300 kgs; RDK-300 - komerční proudový motor, 300 kp)
Tactical-technical data:
Thrust: 2.9-3.4 kN (300-350 kp) 1)/ 3.9 kN (400 kp) 2)
Bypass ratio: 1.0 1) / 2.0 1)
Diameter: 315 mm
Length: 850 mm
Weight: 95 kg
Fuel: T-1 (aviation kerosene / kerosene), T-10 (Decylene)