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Engine Model: RZ.2. Designer: Rolls Royce. Propellants: Lox/Kerosene. Thrust(vac): 836.300 kN (188,008 lbf). Thrust(sl): 735.500 kN (165,347 lbf). Isp: 282 sec. Isp (sea level): 248 sec. Burn time: 156 sec. Mass Engine: 750 kg (1,650 lb). Diameter: 1.53 m (5.00 ft). Chambers: 1. Chamber Pressure: 39.46 bar. Area Ratio: 8.00. Thrust to Weight Ratio: 113.71. Country: UK. First Flight: 1964. Last Flight: 1971. Flown: 22.
RZ.2 used on Rocket Stages
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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