RD R-29R (1)

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Engine Model: RD R-29R (1). Designer: Makeev. Propellants: N2O4/UDMH. Thrust(vac): 682.000 kN (153,319 lbf). Burn time: 74 sec. Country: Russia. RD R-29R (1) used on Rocket Stages Used on stage: R-29-1. on launch vehicle: R-29. 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 - 2008 except where otherwise noted.