An experimental fighter built in response of a government specification, it used a new evaporation cooling system for its V-12 engine, but the system was ineffective at cooling the engine, work ceased in 1939 and instead the I-21 designation was given to Pashinin I-21 (trim for landing gear)
Specifications
General Characteristics
- Created On Windows
- Wingspan 51.4ft (15.7m)
- Length 38.6ft (11.8m)
- Height 16.0ft (4.9m)
- Empty Weight 5,069lbs (2,299kg)
- Loaded Weight 11,032lbs (5,004kg)
Performance
- Horse Power/Weight Ratio 0.09
- Wing Loading 26.8lbs/ft2 (130.6kg/m2)
- Wing Area 412.4ft2 (38.3m2)
- Drag Points 3843
Parts
- Number of Parts 102
- Control Surfaces 8
- Performance Cost 393
@FrankieB thanks
Very nice!