Technology Demonstration
WINGED TEST ROCKET
Mission
Guidance Navigation Control, Composite Propellant Tank, Methane Engine
- Total Length
- 4.60 m
- Total Width
- 2.88 m
- Fuselage Width
- 0.91 m
- Initial Launch Mass
- 1,000 kg
- Propellant
- Liquefied methane / Liquid oxygen (LOX)
- Scheduled Launch Date
- March, 2026
