Lockheed-Pacific F-50E Marlin
Background:
After seeing the success of the F-50 in battle, the United States saw an opportunity to produce a cheap, effective export fighter for its NATO allies using proven designs. Lockheed, under subsidy from the US Government, arranged a production agreement of a new F-50 variant with Pacific Aerospace exclusively for foreign export. The new F-50E had increased engine power, better weapons capability, and folding wings. It was used to great effect by many nations for over 3 decades after its introduction in 1960.
Operators:
Brazil- 35
Israel- 24
Colombia- 20
Republic of Vietnam (South Vietnam)- 12
Iran- 8
Pakistan- 8
Performance:
Unloaded Weight (Full Fuel):10,486 lbs
Max Takeoff Weight (Carrier): 17,000 lbs
Thrust: 13,488 lb/f
Thrust/Weight Ratio (Unloaded): 1.29
Rotation Speed: 180 mph
Stall Speed: 120 mph
Operation:
Taxi below 25 mph
Full Up trim for takeoff
Rotate at 180 mph
Landing approach speed 180 mph
Deploy Drogue Chutes on touchdown for non-carrier landing
Inner Wing/Underbelly hardpoints limited to missiles/rocket pods or drop tank
Deactivate Wing Fold (AG7) before takeoff
Systems:
AG1- Jettison Weapons
AG2- Landing Chute
AG3- Eject
AG4- Jettison Drop Tanks
AG5- Landing Hook
AG7 + VTOL- Fold Wings
AG8- Lights
Specifications
General Characteristics
- Predecessor P-51 Mustang
- Created On iOS
- Wingspan 28.3ft (8.6m)
- Length 25.5ft (7.8m)
- Height 11.9ft (3.6m)
- Empty Weight 5,984lbs (2,714kg)
- Loaded Weight 10,486lbs (4,756kg)
Performance
- Power/Weight Ratio 1.071
- Wing Loading 44.7lbs/ft2 (218.1kg/m2)
- Wing Area 234.8ft2 (21.8m2)
- Drag Points 1864
Parts
- Number of Parts 46
- Control Surfaces 5
- Performance Cost 353