(Performance data
should have been similar to P-38J Model)
CLASSIFICATION
CLASS :
PHOTO-RECONNAISSANCE AIRCRAFT
COUNTRY OF ORIGIN :
UNITED STATES
MANUFACTURER :
Lockheed Aircraft Corporation
FIRST FLIGHT :
1943
SERVICE DELIVERY :
1943
NUMBER BUILT :
200 - F-5B (Converted
from P-38J-5s)
123 - F-5C (Converted
from P-38Js)
100 - F-5E-2 (Converted
from P-38J-15)
5 - F-5E-3 (Converted
from P-38J-25)
500 - F-5E-4 (Converted
from P-38L-1)
SPECIFICATION
SPAN :
52 ft 0 in (15.84 m)
LENGTH :
37 ft 10 in (11.53 m)
HEIGHT :
12 ft 10 in (3.91 m)
WING AREA :
327.5 sq ft (30.42 m sq)
WING LOADING :
---
POWER LOADING :
---
ASPECT RATIO :
---
WEIGHT EMPTY :
12,780 lbs (5797 kg)
WEIGHT LOADED :
17,500 lbs (7938 kg)
WEIGHT MAX :
21,600 lbs (9798 kg)
ARMAMENT :
1 x 20 mm Cannon,
4 x .50-cal Machine Guns
PAYLOAD :
3,200 lbs (1451 kg) of Bombs
POWER PLANT :
2 x Allison V-1710-89/91 Turbo-Supercharged Piston Engines, Rated
at 1,425 hp each
CREW :
1 - Pilot
PERFORMANCE
MAXIMUM SPEED :
414 mph (666 km/h) at 25,000 ft (7620 m)
CRUISING SPEED :
290 mph (467 km/h)
LANDING SPEED :
105 mph (169 km/h)
CLIMB RATE :
To 20,000 ft (6096 m) in 7 min
RANGE :
450 miles (724 km); 2,600 miles (4184 km) Max
SERVICE CEILING :
44,000 ft (13411 m)
REFERENCES
Angelucci, Enzo; Bowers, Peter. The American Fighter - The Definitive Guide To American Fighter Aircraft From 1917 to the Present. New York: Orion Books. 1985. ISBN 0-517-56588-9.