Low-cost, ablative, pressure-fed, LOX/kerosene rocket engine
Features
- Composite chamber
- Mixture ratio, 2.25
- Designed for Jet A
- Area ratio, 6.56 (4.1 to 80)
- Chamber pressure, 390 psi
- Altitude version available
- Able to be gimbaled 15 deg
- Replaceable chamber
- Very simple interfaces and operations
- Extendible to 9K lbf, low-pressure version
Applications
- All stages of launch vehicles
- Liquid boosters
- Expendable upper stages
- Suborbital vehicles including targets
- Reusable booster demonstrators
- Research vehicles
- Experimental vehicles
- Scalable to much higher thrust levels
SCORPIUS 20K lbf Engine
POINT OF CONTACT
For technical details and quote,
please contact:
Dr. Nicola Sarzi-Amade
310-219-2700
namade@scorpius.com