NagaTomo Space Tourism Spaceplane
Crewed suborbital spaceplane for commercial space travel, carrying 2 crew and 6 passengers to 120 km altitude, targeted for 2030.
Technical specifications
- Total Length
- 17.7 m
- Total Width
- 12.3 m
- Fuselage Length
- 15.8 m
- Fuselage Width
- 2.95 m
- Main Wing Reference Area
- 41.9 m²
- Mean Aerodynamic Chord (MAC)
- 4.24 m
- Propellant
- LBM (Liquefied Biomethane) / LOX (Liquid Oxygen)
- Altitude
- 120 km
- Crew
- 2 people
- Passengers
- 6 people
- Scheduled Launch Date
- 2030
- Mission
- Space Travel
About
NagaTomo is SPACE WALKER’s crewed suborbital spaceplane designed for commercial space travel, targeted for service entry in 2030. It carries a crew of 2 and up to 6 passengers to an altitude of 120 km. NagaTomo shares the same airframe dimensions as the FuJin/RaiJin vehicle: 17.7 m total length, 12.3 m total width (wingspan), 15.8 m fuselage length, 2.95 m fuselage width, 41.9 m² main wing reference area, and a 4.24 m mean aerodynamic chord. It is propelled by liquefied biomethane (LBM) and liquid oxygen (LOX), reflecting SPACE WALKER’s carbon-neutral propulsion strategy across its winged reusable rocket family.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
