This is a simple EF-2000 "Typhoon" fighter. It took me three days to manufacture it. The operation method is as follows: AG-1: VTOL max: Deceleration flap .AG-2: VTOL max: Open afterburner.AG- 8: Main engine.considerations: 1. The stall speed of this aircraft is about 55 mph, please do not land at a speed lower than 55 mph. 2. Please do not let the nose point too far from the target when launching a missile, otherwise the missile May not hit the target. S.P.F. Design Bureau & Air Trane Design Bureau produced. Have a good time! #^_^#
Specifications
General Characteristics
- Created On Android
- Wingspan 31.5ft (9.6m)
- Length 44.2ft (13.5m)
- Height 14.6ft (4.4m)
- Empty Weight N/A
- Loaded Weight 13,467lbs (6,108kg)
Performance
- Power/Weight Ratio 6.007
- Wing Loading 22.6lbs/ft2 (110.3kg/m2)
- Wing Area 596.1ft2 (55.4m2)
- Drag Points 7701
Parts
- Number of Parts 112
- Control Surfaces 7
- Performance Cost 784
