AJ10-33
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet Nitric acid/UDMH rocket engine. SMART Sled. Development begun early 1950s. 114,000 lbf thrust, uncooled, ceramic lined, 3 chamber system
Propellant Formulation: IRFNA/UDMH.
Subtopics
- AJ10-51 Aerojet rocket engine. Sled. Thrust variable to 33% indicated.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- Nitric acid/UDMH
- Agency
- Aerojet