The TS-140 was a canard type aircraft to be powered by four Bristol Orpheus jet engines. The US selected the Bell D-188A proposal instead.
Specifications
General Characteristics
- Successors 3 airplane(s) +28 bonus
- Created On iOS
- Wingspan 21.1ft (6.4m)
- Length 44.3ft (13.5m)
- Height 10.9ft (3.3m)
- Empty Weight 10,849lbs (4,921kg)
- Loaded Weight 22,034lbs (9,994kg)
Performance
- Power/Weight Ratio 2.039
- Wing Loading 133.2lbs/ft2 (650.3kg/m2)
- Wing Area 165.4ft2 (15.4m2)
- Drag Points 2817
Parts
- Number of Parts 28
- Control Surfaces 1
- Performance Cost 237
