Suborbital spaceplane for science missions (FuJin) and small satellite launch to LEO/SSO (RaiJin), targeting a 2028 debut from Taiki, Hokkaido.
FuJin/RaiJin Suborbital Spaceplane
Suborbital spaceplane for science missions (FuJin) and small satellite launch to LEO/SSO (RaiJin), targeting a 2028 debut from Taiki, Hokkaido.
Description
FuJin/RaiJin is SPACE WALKER's suborbital winged reusable spaceplane, planned for launch in March 2028 from Taiki, Hokkaido. In its FuJin science-mission configuration it reaches an altitude of 150 km; in its RaiJin satellite-launch configuration it delivers approximately 310 kg to a 600 km LEO or 310 kg to a 600 km sun-synchronous orbit (SSO). The vehicle measures 17.7 m in total length, 12.3 m in total width (wingspan), with a 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), with an initial launch mass of 43,397 kg. The RaiJin configuration adds a first upper stage (1,558 kg dry / 11,266 kg total) and a second upper stage including fairing and payload (888 kg dry / 3,189 kg total), for a combined initial launch mass of 57,852 kg.
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 Bio-Methane) / LOX (Liquid Oxygen) |
| Initial Launch Mass | 43,397 kg |
| First Upper Stage (RaiJin) Dry Mass | 1,558 kg |
| First Upper Stage (RaiJin) Total Mass | 11,266 kg |
| Second Upper Stage (RaiJin) Dry Mass | 888 kg (incl. fairing and payload) |
| Second Upper Stage (RaiJin) Total Mass | 3,189 kg |
| Combined Initial Launch Mass (RaiJin) | 57,852 kg |
| Scheduled Launch Date | March 2028 |
| Launch Site | Taiki, Hokkaido, Japan |
| Mission (FuJin) | Science mission, altitude 150 km |
| Mission (RaiJin) | 310 kg to LEO (600 km) or 310 kg to SSO (600 km) |