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LR-105-3
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Government Designation: LR105-3. Designer: Rocketdyne. Propellants: Lox/Kerosene. Thrust(vac): 375.000 kN (84,303 lbf). Thrust(sl): 267.000 kN (60,023 lbf). Isp: 308 sec. Isp (sea level): 220 sec. Chambers: 1. Chamber Pressure: 50.30 bar. Oxidizer to Fuel Ratio: 2.27. Country: USA. Status: Out of Production. Early version of Atlas Sustainer. Gas generator, pump-fed.
Bibliography and Further Reading - Kudryavtseva, V M, ed., Zhidkostnikh Raketnikh Dvigatley, Visshaya Shkola, Moscow, 1993. ISBN: 5060025632. Russian-language textbook on rocket theory. More at amazon.com...
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