30AL-1000
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 March 1947. Boeing surface-to-air missile, which would evolve into Bomarc and reach IOC in 1959.
Thrust (sl): 4.410 kN (991 lbf). Thrust (sl): 450 kgf. Propellant Formulation: Nitric acid/Aniline.
Related
- Family
- Storable liquid
- Country
- USA
- Launch Vehicles
- Bomarc
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet