Aerobee 150A-2
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet ntric acid/Amine propellant rocket stage. Typical ideal dV=3839 m/s; gravity and drag losses = 1012 m/s.
Nitric acid/Aniline engine.
Related
- Family
- Storable liquid
- Country
- USA
- Engines
- AJ11-6
- Launch Vehicles
- Aerobee 150A
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet