LR2-RM-6

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Engine Model: LR2-RM-6. Designer: Fairchild. Gross Mass: 500 kg (1,100 lb). Propellants: Liquid. Thrust(vac): 2.800 kN (629 lbf). Burn time: 260 sec. Diameter: 0.46 m (1.50 ft). Length: 4.20 m (13.70 ft). Country: USA. LR2-RM-6 used on Rocket Stages Used on stage: Lark. on launch vehicle: Lark. 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.