45AL-2600
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet Nitric acid/Amine rocket engine. Development begun June 1948. Manufacture of complete Aerobee systems First flight 1955.
Thrust (sl): 11.700 kN (2,630 lbf). Thrust (sl): 1,200 kgf. Propellant Formulation: RFNA/Aniline+Furfural Alcohol.
Related
- Family
- Storable liquid
- Country
- USA
- Launch Vehicles
- Aerobee Hi
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet