Scimitar Rocket Engine
1,200 lbf thrust main engine currently powering the Xodiac vehicle — 100+ successful flights, 35,000+ seconds of total operation, LOX/isopropyl alcohol propellants.
Technical specifications
- Thrust
- 1,200 lbf
- Propellants
- Liquid Oxygen / Isopropyl Alcohol
- Flight heritage
- 100+ successful flights, 35,000+ seconds of operation
- Chamber material options
- Copper or aluminum
- Vehicle application
- Xodiac
About
Scimitar is Masten’s 1,200 lbf thrust rocket engine, currently in use as the main engine on the Xodiac vehicle. It has powered more than 100 successful flights with over 35,000 seconds of total operation. The engine can be configured with either a copper or aluminum combustion chamber and evolved from the earlier Hatchet engine design.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.