Bell P-39 Airacobra
One of the first "modern" Air Corps fighter designs and the first fighter
designed by Bell, Airacobras were used primarily for ground attack. The XP-39 prototypes
featured an engine supercharger, but the Army's decision to eliminate it on production
aircraft greatly limited the type's effectiveness, and, in fact, the aircraft performed
best below 17,000 ft. The P-39 had a unique automobile-type cockpit door, tricycle landing
gear (another first for an AAC fighter), and a center-fuselage-mounted engine. The
Airacobra entered Air Corps service in 1941. At the time of the Japanese attack on Pearl
Harbor, 179 British Airacobras were still in the US waiting to be delivered, and these
aircraft were commandeered by the AAC, redesignated P-400, and sent to the southwest
Pacific. US P- 39s were used extensively in operations in North Africa (most particularly
Operation Torch), Italy, and the Pacific. The type achieved the lowest loss rate per
sortie of any Army Air Forces fighter used in the European theater of operations, although
it was mostly used in areas where Bf-109s and FW-190s were scarce. Numerous P-39s remained
in the US during the war, where they were used for training units.
Almost half of the production run was sent to the Soviet Union, where its tank-killing
capability was used to great advantage. Most of these aircraft were ferried to Russia via
Alaska. P-39s were also flown in numbers by the RAF and the Free French. Production ended
in August 1944. Several aircraft were used by NACA as research aircraft at the Ames Flight
Research Center in California, and a number were flown as racers after the war, but only a
handful of P-39s are still in existence.
The larger, better-performing P-63 Kingcobra was a direct descendent of the P-39.
General characteristics P-39D |
Primary function |
Fighter |
Contractor |
Bell Aircraft Corp. |
Power plant |
One Allison V-1710-35 engine |
Thrust |
1,609 HP |
1,200 kW |
Wingspan |
34 ft |
10.37 m |
Length |
30.2 ft |
9.21 m |
Height |
11.8 ft |
3.60 m |
Wingarea |
213 sq ft |
19.79 sq m |
Weight |
empty |
6,305 lb |
2,860 kg |
max. |
8,860 lb |
4,018 kg |
Max. speed |
335 mph |
539 km/h |
Ceiling |
32,100 ft |
9,785 m |
Max. range |
1,100 miles |
1,770 km |
Armament |
1x 37mm cannon (60 rounds), 4x 7.62mm machine guns, 2x 12.7mm machine
guns, 1x 227 kg bomb. |
Crew |
One |
First flight |
April 6, 1938 (XP-39) |
Date deployed |
1941 |
General characteristics P-39N |
Primary function |
Fighter |
Power plant |
One Allison V-1710-85 liquid-cooled V-12 engine |
Thrust |
1,609 HP |
1,200 kW |
Wingspan |
34 ft |
10.37 m |
Length |
30.2 ft |
9.21 m |
Height |
12.4 ft |
3.79 m |
Wingarea |
213 sq ft |
19.79 sq m |
Weight |
empty |
6,407 lb |
2,906 kg |
max. |
8,807 lb |
3,995 kg |
Speed |
376 mph |
605 km/h |
Initial climb rate |
4,000 ft/min |
1,220 m/min |
Ceiling |
35,000 ft |
10,670 m |
Range |
normal |
976 miles |
1,570 km |
2 ext. tanks |
1,446 miles |
2,360 km |
Armament |
1x 37mm cannon, 2x 7.62mm machine guns, 2x 12.7mm machine guns, 1x 227 kg
bomb. |
Crew |
One |
Cost |
$46,000 |
Number built |
9,558 (all types) |
Jirka Wagner
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