LR87-9
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet N2O4/Aerozine-50 rocket engine. Variant of LR-87 used on early versions of Titan III B,C First flight 1966.
Thrust (sl): 956.100 kN (214,940 lbf). Thrust (sl): 97,500 kgf.
Related
- Family
- Storable liquid
- Country
- USA
- Launch Vehicles
- Titan IIIC, Titan IIIB
- Propellants
- N2O4/Aerozine-50
- Agency
- Aerojet