LR87-3
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: Bob Fortune
Aerojet LOx/Kerosene rocket engine. Titan 1 booster engine. Surplus Flight Engines were available for various uses in the 1960's. First flight 1959.
Thrust (sl): 647.900 kN (145,654 lbf). Thrust (sl): 66,067 kgf. Engine: 839 kg (1,849 lb). Chamber Pressure: 40.00 bar. Area Ratio: 8. Thrust to Weight Ratio: 89.204410011919. Oxidizer to Fuel Ratio: 1.91. Coefficient of Thrust vacuum: 1.84532204931916. Coefficient of Thrust sea level: 1.64532204931916.
Related
- Country
- USA
- Launch Vehicles
- Titan I, Super-Jupiter, Juno V-A, Juno V-B, Saturn A-1
- Propellants
- Lox/Kerosene
- Stages
- Titan 1-1
- Agency
- Aerojet