21AL-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 January 1946. Regeneratively cooled. Development and production first flight 1953.
Thrust (sl): 11.700 kN (2,630 lbf). Thrust (sl): 1,200 kgf. Propellant Formulation: Nitric acid/Aniline.
Related
- Family
- Storable liquid
- Country
- USA
- Launch Vehicles
- Nike Ajax
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet