Aerobee 150-2
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet nitric acid/Aniline propellant rocket stage. Thrust 17.80 kN.
Subtopics
- Aerobee 150A-2 Aerojet ntric acid/Amine propellant rocket stage. Typical ideal dV=3839 m/s; gravity and drag losses = 1012 m/s.
Related
- Family
- Storable liquid
- Country
- USA
- Engines
- AJ11-6
- Launch Vehicles
- Aerobee Hi, Aerobee, Aerobee 300, Aerobee 150, Aerobee 300A, Aerobee 150 MI, Aerobee 170, Aerobee 170B, Aerobee 170A, Aerobee 150A MII
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet