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Manufacturer: Lockheed Aircraft Corporation, USA 1939
Powerplant: . (P-38J) Two 1,425 hp (1063 kw) Allison V-1710-89/91 inline piston engines (higher rated due to an improved cooling system). Under war emergency conditions 1,600 hp
(1193 kW) was available at altitude.
Performance: Maximum speed 414 mph (666 km/h) at 25,000 ft (7620 m); cruising speed 290 mph (467 km/h); service ceiling 44,000 ft (13410 m).
Range: 475 miles (764 km) at 339 mph (545 km/h) at 25,000 ft (7620 m). Maximum range was 2260 miles (3638 km) at 186 mph (299 km/h) at 10,000 ft (3048 m) with two 250 Imp
gallon drop tanks.
Weight: Empty 12,780 lbs (5797 kg), Normal 17,500 lbs (7936 kg) with a maximum take-off weight of 21,600 lbs (9798 kg).
Dimensions: Span 52 ft 0 in (15.85 m); length 37 ft 10 in (11.53 m); height 9 ft 10 in (3.00 m); wing area 327.5 sq ft (30.42 sq m).
Armament: One 20 mm Hispano M2(C) cannon with 150 rounds plus four 12.7 mm (0.50 in) Colt-Browning MG 53-2 machine guns with 500 rounds per gun. In addition two 500 lbs
(227 kg), 1,000 lbs (454 kg), or 1600 lbs (726 kg) bombs or ten five-inch rockets could be carried on underwing racks.
45
23
7
11
31
8
5
11a
33
2
24
28
29
1
25
30
10
11A
11C
33
9
22a+22b
42
11E
1
16
38
36
39
41
11B
12
40
37+37A
34+34A+35
12
32
11D
43
14,15
32
45
13
30b
11
28
25
30a
33
27
23a
26
30
11
22a+
22b
29
31
1
39
R
2
12
12
40
3
L
37
38
14
15
37A
13
13
8
37A
37A
37A
4
7
36
5
45
41
6
30
30a
43
L
31
9
16
10
a
b
c
d
31
R
44
44a
30b
19
29
17
19A
18
28
L
20
21
35
22b
23
34
29A
22
22a
32
33
23a
24
26
29A
27
42
25
11
11a
29
19
19A
17
28
18
R
20
21
35
22b
29A
34
23
32
22a
22
33
23a
24
26
29A
27
42
11
25
C
E
C
D
F
A
A
B
B
F
Part of wire
I
x 2
II
x 1
8
7
E
11A
Weight
3
5
10
2
B
6
38
36
39
9
F
34+34A+35
1
A
C
4
D
5
37+37A
II
16
WIRE
18
25
24
17
26
29A
23
17A
11
18B
20A
20B
17B
24A
29
25A
30
19A
18A
20
21A
I
19
22
21
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Manufacturer: Lockheed Aircraft Corporation, USA 1939
Powerplant: . (P-38J) Two 1,425 hp (1063 kw) Allison V-1710-89/91 inline piston engines (higher rated due to an improved cooling system). Under war emergency conditions 1,600 hp
(1193 kW) was available at altitude.
Performance: Maximum speed 414 mph (666 km/h) at 25,000 ft (7620 m); cruising speed 290 mph (467 km/h); service ceiling 44,000 ft (13410 m).
Range: 475 miles (764 km) at 339 mph (545 km/h) at 25,000 ft (7620 m). Maximum range was 2260 miles (3638 km) at 186 mph (299 km/h) at 10,000 ft (3048 m) with two 250 Imp
gallon drop tanks.
Weight: Empty 12,780 lbs (5797 kg), Normal 17,500 lbs (7936 kg) with a maximum take-off weight of 21,600 lbs (9798 kg).
Dimensions: Span 52 ft 0 in (15.85 m); length 37 ft 10 in (11.53 m); height 9 ft 10 in (3.00 m); wing area 327.5 sq ft (30.42 sq m).
Armament: One 20 mm Hispano M2(C) cannon with 150 rounds plus four 12.7 mm (0.50 in) Colt-Browning MG 53-2 machine guns with 500 rounds per gun. In addition two 500 lbs
(227 kg), 1,000 lbs (454 kg), or 1600 lbs (726 kg) bombs or ten five-inch rockets could be carried on underwing racks.
45
23
7
11
31
8
5
11a
33
2
24
28
29
1
25
30
10
11A
11C
33
9
22a+22b
42
11E
1
16
38
36
39
41
11B
12
40
37+37A
34+34A+35
12
32
11D
43
14,15
32
45
13
30b
11
28
25
30a
33
27
23a
26
30
11
22a+
22b
29
31
1
39
R
2
12
12
40
3
L
37
38
14
15
37A
13
13
8
37A
37A
37A
4
7
36
5
45
41
6
30
30a
43
L
31
9
16
10
a
b
c
d
31
R
44
44a
30b
19
29
17
19A
18
28
L
20
21
35
22b
23
34
29A
22
22a
32
33
23a
24
26
29A
27
42
25
11
11a
29
19
19A
17
28
18
R
20
21
35
22b
29A
34
23
32
22a
22
33
23a
24
26
29A
27
42
11
25
C
E
C
D
F
A
A
B
B
F
Part of wire
I
x 2
II
x 1
8
7
E
11A
Weight
3
5
10
2
B
6
38
36
39
9
F
34+34A+35
1
A
C
4
D
5
37+37A
II
16
WIRE
18
25
24
17
26
29A
23
17A
11
18B
20A
20B
17B
24A
29
25A
30
19A
18A
20
21A
I
19
22
21
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