A fully reusable spacecraft designed for interplanetary travel, capable of carrying large crews and cargo.
Specifications
- Height: 120 m
- Diameter: 9 m
- Mass: 5,000 t
- Payload To Leo: 150 t
- Propellant: Liquid methane/oxygen
- Crew Capacity: 100
- Speed: 7.8 km/s
- Fuel Efficiency: 0.5
- Base Cost: $90M
- Landing Method: Vertical propulsive landing
Launch History
First orbital flight in 2024, multiple lunar missions by 2025.