Unit
type: prototype non-transformable drone fighter
Manufacturer: Mars Base
Total dry weight: 16.70 tons
Total length: 10.25 meters
Total height: 3.60 meters
Total wingspan: 6.40 meters
Primary engines: JG-97M liquid hydrogen cell turbine (producing 1840shp each) x 2
Secondary engines: ATF-401 (producing 4800kg of thrust each) x 4
Fuel capacity: standard HBT cell (4-pak x 4)
HBT supply: 250 hours (10 days) operational use
Delta-V (space): 1.8 kps with internal reaction mass
Max. level speed (sea level): 1100 km/h (Mach 1.0)
Max. level speed (18000 meters): 2465 km/h (Mach 2.3)
Stall speed: 182 km/h (VTOL rectification possible)
Initial climb rate: over 20000 meters per minute
Unboosted service ceiling: 26000 meters
Fixed armament: MM-24 multimissile system: 8-tube upper fuselage launcher x 2, 4-tube lower fuselage launcher x 2