The General Motors/Fisher P-75 Eagle was a fighter aircraft designed by the Fisher Body Division of General Motors. Development started in September 1942 in response to United States Army Air Forces requirement for a fighter possessing an extremely high rate of climb, using the most powerful liquid-cooled engine then available, the Allison V-3420. The program was cancelled after only a small number of prototypes and production aircraft had been completed, as it was no longer required in its original role, could not be quickly deployed, and possessed no significant advantages over aircraft already in production
Specifications
General Characteristics
- Created On Windows
- Wingspan 38.5ft (11.8m)
- Length 32.9ft (10.0m)
- Height 11.6ft (3.5m)
- Empty Weight 7,185lbs (3,259kg)
- Loaded Weight 9,944lbs (4,510kg)
Performance
- Horse Power/Weight Ratio 0.201
- Wing Loading 41.7lbs/ft2 (203.7kg/m2)
- Wing Area 238.4ft2 (22.1m2)
- Drag Points 4572
Parts
- Number of Parts 107
- Control Surfaces 5
- Performance Cost 508
@CPwaffles4240 well the last P75 is in the museum's Experimental Aircraft Gallery.
@coolhand83 when you take off first pull down the left control first,then pitch
Can't take off.... the pitch is very difficult to handle and it yaws for fun on the ground :(
@Liquidfox lol,wish you like her
@VernalTie513 thank you:)
Noice :D