Overview: the H800 is an experimental transport aircraft, featuring a rear engine nacelle that houses 5 TJE-1 turbojet engines, which are fed by the large ring-shaped inlet surrounding the fuselage.
Maximum Airspeed (TAS): 700mph, 1127kph, 608knots.
Maximum Altitude: 40,000ft, 12,192m.
Cruise Altitude: 15,000-35,000ft, 4,572-10,668m.
Cruise Airspeed (TAS): 500-675mph, 805-1086kph, 435-587knots (depending on altitude).
Takeoff Airspeed (IAS): 135mph, 217kph, 117knots.
Cruise Power: 25-75% (depending on altitude).
Controls: VTOL: Flaps.
Notes: the 5 turbojet engines can easily push the aircraft beyond Mach 1 at higher altitudes if you're not careful.
Specifications
General Characteristics
- Created On Windows
- Wingspan 79.0ft (24.1m)
- Length 60.1ft (18.3m)
- Height 18.2ft (5.5m)
- Empty Weight 29,021lbs (13,164kg)
- Loaded Weight 36,289lbs (16,460kg)
Performance
- Power/Weight Ratio 1.548
- Wing Loading 49.4lbs/ft2 (241.2kg/m2)
- Wing Area 734.6ft2 (68.3m2)
- Drag Points 6291
Parts
- Number of Parts 49
- Control Surfaces 7
- Performance Cost 323
