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United States' Bell P-39 Airacobra fighter1,2,3,4,5
Bell P-39 Airacobra:
Bell P-39 Airacobra used by the Soviets:
Bell P-63 Kingcobra and Bell P-39 Airacobra used by the Soviets:
Design
The Bell P-39 Airacobra was designed around the 37 mm T-9 cannon that was demonstrated in 1935.2,4,5
Engine
By using this gun the engine had to be placed in the middle of the fuselage and the drive shaft ran under the pilot's seat.1,2,3,4,5
Landing Gear
It also had a tricycle undercarriage which was a first for a operational fighter.1,4
Cockpit
The P-39's pilot was well protected by armor.1 The cockpit door opened similarly to a car door.1
Prototype
The XP-39 made it's first flight on April 6, 19383 / April 6, 19391,2,5.4
Production
Production went on until May 1944.4
- XP-39: 14
- XP-39E: 34
- YP-39: 134
- P-39C: 203,4
- P-39D: 9234
- Airacobra I: 4974
- P-39J: 253, 294
- P-39K: 2104
- P-39L: 2504
- P-39M: 2404
- P-39N: 2,0953,4
- P-39N and P-39Q: 2,0952
- P-39Q: 4,9053,4
- P-49F: 2294
- P-400: 1794
- Total: 9,5581,2,3,5, 9,5944
Variants
- Naval XFL-1: Naval variant with a tail wheel and arrester hook. Wasn't successful in trials.1
- V-Tail: Experimental tail that had combined elevator and rudder functions.1 Reduced the P-39's handling.1
- XP-39: Prototype.2,5
- XP-39E: It had a square tail which was similar to a P-51.1 Powered by an Allison V-1710-47.1 Had laminated flow wings.3,4
- YP-39: Thirteen were built for evaluation.3 Had an engine mounted 37 mm cannon, two fuselage mounted 12.7 mm guns, and two wing mounted 7.62 mm.3
- P-39C: Initial production model that was basically the same as the YP-39.3
- P-39D: Production model that entered service in 19412,4,5 / February 19423. Used Curtis propellar.2 Added self sealing fuel tanks, and two more wing mounted 7.62 mm MGs.3
- P-39D-1 / Airacobra I: Used a 20 mm M1 instead of the 37 mm M4.3
- P-39D-2: Used V-1710-63 (1,325 HP) engine.3
- P-39F: Used Aeroproducts propellar.2,5
- P-39J: Used V-1710-59 engine.2,3,5 1,100 HP.3
- P-39K: Used V-1710-63 engine.2,5 Used the Aeroproducts propellar.5
- P-39L: Used V-1710-63 engine with Curtis propellar.2,5 New nosewheel.3
- P-39M: Used V-1710-83 engine and a large diameter propellar.2,3,5 1,200 HP.3 Started to be used in November 1942.3
- P-39N: Used V-1710-85 engine.2,3,5 1,200 HP.3
- P-39Q: Used V-1710-85 engine.2,5 Wing guns were removed and 12.7 mm MGs were mounted beneath the wings.3
Usage
Australia, Britain, France, Italy, Portugal, Soviet Union, United Kingdom, and the United States used the P-39.4
French Order
France ordered some P-39s but they were taken over by the United Kingdom.4
Royal Air Force Disappointed
The RAF tested the P-39 but it didn't perform up to the standards of the British fighters at the time.1 However, 675 were ordered, but only the No. 601 Squadron2,5 received them.1 250 of them were sent to the Soviet Union.4
Fighting With the United States
The United States needed to use any available fighters against Japan in 1942 and 1943 and in the early combat in the Middle East.1
The first combat was in April 1942 against the Japanese.5
"Shaving" With the Soviet Union
Approximately 5,000 (4,7732,5) were supplied to the Russians and they were nick named "Shaving" as it was slang for ground strafing.1 It was well liked for its ability to destroy German vehicles.1
Free French and Italian Co-Belligerent
Some French and Italian pilots (of the Italian co-belligerent Air Force in 1944) also flew the P-39.1
Australians
The Australians used 22 P-39s.44
| Bell XP-393 | Bell P-39 Airacobra1 | Bell P-39D Airacobra3 | Bell P-39N Airacobra2,5 | Bell P-39Q Airacobra4 | |
|---|---|---|---|---|---|
| Type | Fighter1 Fighter bomber4 |
Fighter2,5 | |||
| Crew | 11,4 | 12,5 | |||
| Engine (Type) | Allison V-1710-173 | Allison V-1710-631 | Allison V-1710-354 | Allison V-1710-854 piston2,5 | |
| Cylinders | 123 | V 124 | Inline2 V 125 |
||
| Cooling | Liquid3 | Liquid1 | |||
| HP | 1,1503 | 1,2001 | 1,1504 | 1,2002,4 | |
| Propeller blades | 34 | ||||
| Dimensions | |||||
| Span | 34'1,4 10.36 m1,4 |
34'3 10.36 m3 |
34'2,5 10.36 m2,5 |
||
| Length | 30'1, 30' 2"4 9.19 m1,4 |
30' 2"3 9.19 m3 |
30' 2"2,5 9.19 m2,5 |
||
| Height | 11' 10"4, 12'1 3.6 m4, 3.78 m1 |
11' 10"3 3.6 m3 |
12' 5"2,5 3.78 m2,5 |
||
| Wing area | 213 ft2 1 19.79 m2 1 |
213 ft2 3 19.79 m2 3 |
213 ft2 2,3 19.79 m2 2,3 |
||
| Weight | |||||
| Empty | 5,645 lb1 2,566 kg1 |
5,462 lb3 2,477 kg3 |
5,657 lb2,5 2,566 kg2,5 |
5,645 lb4 2,560 kg4 |
|
| Loaded | 8,145 lb1 3,702 kg1 |
8,850 lb3 4,014 kg3 |
8,200 lb2,5 3,720 kg2,5 |
8,300 lb4 3,765 kg4 |
|
| Performance | |||||
| Speed | 400 mph1 642 kph1 |
||||
| Speed @ 5,000' / 1,524 m |
335 mph3 539 kph3 |
||||
| Speed @ 9,700' / 2,955 m |
399 mph2,5 642 kph2,5 |
||||
| Speed @ 11,000' / 3,350 m |
385 mph4 620 kph4 |
||||
| Speed @ 13,800' / 4,200 m |
368 mph4 592 kph4 |
||||
| Speed @ 15,000' / 4,572 m |
360 mph3 579 kph3 |
||||
| Climb to 15,000' / 4,570 m |
3.8 minutes2,5 | 4.5 minutes4 | |||
| Climb to 15,000' / 4,575 m |
5.7 minutes4 | ||||
| Service ceiling | 38,500'1 11,735 m1 |
32,100'4 9,785 m4 |
38,500'2,5 11,735 m2,5 |
35,000'4 10,670 m4 |
|
| Range | 750 miles1 1,207 km1 |
800 miles4 1,287 km4 |
750 miles2,5 1,207 km2,5 |
650 miles4 1,046 km4 |
|
| Range - internal @ 300 mph / 483 kph @ 25,000' / 7,620 m |
450 miles3 724 km3 |
||||
| Armament | |||||
| Propeller hub | 1: 37 mm M41 30 rounds1 |
1: 37 mm4 | 1: 37 mm2,4,5 | ||
| Nose | 2: 12.7 mm1 | 2: 0.5"4 | 2: 12.7 mm2,4,5 | ||
| Wings | 4: 7.62 mm MG1 | 2 or 4: 0.3" MG4 | 4: 7.62 mm MG2,5 2 or 4: 0.3" MG4 |
||
| Under wing | 2: 12.7 mm1,4 | ||||
| Bombs - under fuselage | 500 lb1 227 kg1 |
1: 500 lb2,5 1: 227 kg2,5 |
|||
| Bombs | 1: 500 lb4 1: 227 kg4 |
1: 500 lb4 1: 227 kg4 |
Sources:
- Aircraft of WWII, General Editor: Jim Winchester, 2004
- Fighting Aircraft of World War II, Editor: Karen Leverington, 1995
- The Great Book of Fighters, William Green, Gordon Swanborough, 1994
- Aircraft of WWII, Stewart Wilson, 1998
- The Encyclopedia of Weapons of World War II, General Editor Chris Bishop, 1998
