LR87-11 AJ23-138
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet N2O4/Aerozine-50 rocket engine. Version of LR-87-11 tuned for launch pad ignition when used on Titan 3B. First flight 1966.
Thrust (sl): 1,008.310 kN (226,677 lbf). Thrust (sl): 102,820 kgf.
Related
- Family
- Storable liquid
- Country
- USA
- Launch Vehicles
- Titan IIIB
- Propellants
- N2O4/Aerozine-50
- Agency
- Aerojet