Bell P-39 Airacobra

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by DocWatson42 (talk | contribs) at 03:52, 19 June 2007 (Changed a hyphen to an en dash.). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Template:Infobox Aircraft

The Bell P-39 Airacobra was one of the principal American fighter aircraft in service at the start of World War II. Although its mid-engine placement was innovative, the P-39 design was handicapped by the lack of an efficient turbo-supercharger, limiting it to low-altitude work, although the type was utilized with great success by the Soviet Air Force. Together with the derivative P-63 Kingcobra, these aircraft would be the most successful mass-produced, fixed-wing aircraft manufactured by Bell.

Design and development

The P-39 made its initial flight in April 1939 at Wright Field, Ohio. In 1937, the Army Air Corps issued a specification for a new fighter that could be produced quickly. The Curtiss P-40 was a growth of a previous design, while Lockheed's P-38 used twin booms. Bell's P-39 adopted an unique configuration with its V-12 Allison engine mounted in the middle of the fuselage, just behind the cockpit. The propeller was driven through a driveshaft passing between the pilot's feet. The main purpose of this configuration was to free up space for the heavy main armament, a 37 mm T9 cannon firing through the center of the propeller hub for optimum accuracy and stability when firing. Although a devastating weapon, it was prone to jamming.[citation needed] A secondary benefit of the mid-engine arrangement was to create a smooth and streamlined nose profile. The weight distribution necessitated a tricycle undercarriage, a first among American fighters. Entry to the cockpit was through side doors (mounted on both sides of the cockpit) rather than a sliding canopy. Its unusual engine location behind the cockpit caused some pilot concern at first, but experience showed that this was no more of a hazard in a crash landing than with an engine located forward of the cockpit.

The weight distribution of the P-39 supposedly is the reason for its tendency to enter a dangerous flat spin — a characteristic Soviet test pilots were able to demonstrate to the then-skeptical manufacturer who had been unable to reproduce the effect. After extensive tests, it was determined that the spin could only be induced if the plane was improperly loaded, with no ammunition in the front compartment. The flight manual specifically noted that one had to ballast the front ammunition compartment with the appropriate weight of shell casings to achieve a reasonable center of gravity. High speed controls were light ala P-51, thus high speed turns and pull-outs were not the strength test of a P-40 or P-47, never mind the Zero or Me 109. The P-39 had to be held in a dive since it wanted to level out, reminiscent of the Spitfire. Redline dive speed was a respectable 525 mph for the P-39 'Cobra.

Bell P-39 Airacobra center fuselage detail with maintenance panels open.

The P-39's Allison V-1710 engine had a single-speed, single-stage supercharger, which brought about a decrease of performance compared to the promising prototype fitted with an exhaust-driven turbo-supercharger. The production P-39's heavier weight combined with the poor performance of the Allison engine, limited the high-altitude capabilities of the fighter. The P-39's altitude performance was markedly inferior to the contemporary European fighters and, as a result, the first USAAF fighter units in the European Theater were equipped with the Spitfire V (which coincidentally also featured a single-speed, single-stage supercharger). However, the P-39D's roll rate was 75 degrees per second at 235 mph– better than the A6M2, F4F, F6F or P-38 up to 265 mph. see NACA chart).[citation needed]

Above the V-1710's full throttle height of about 17,000 ft (5,000 m), the P-39's performance dropped off rapidly. This limited its usefulness in traditional fighter missions in Europe as well as in the Pacific, where it was not uncommon for Japanese bombers to attack at altitudes above the P-39's operational ceiling (which in the tropical hot air inevitably was lower than in moderate climates).

A naval version with taildragger landing gear, the XFL-1 Airabonita, was ordered as a competitor to the F4U Corsair and XF5F Skyrocket, but after a troublesome and protracted development and testing period, was rejected by the Navy.

By the time of the Pearl Harbor attack, nearly 600 had been built. When P-39 production ended in August 1944, Bell had built 9,584 Airacobras, of which 4,773 were sent to the Soviet Union through the Lend-Lease program.

The mid-engine, gun-through-hub concept was developed further in the Bell P-63 Kingcobra.

Operational history

The Airacobra saw combat throughout the world, particularly in the Southwest Pacific, Mediterranean and Russian theaters. Because its engine was not equipped with a supercharger, the P-39 performed best below 17,000 feet altitude. It often was used at lower altitudes for such missions as ground strafing.

Russian pilots appreciated the cannon-armed P-39 for its ground attack capability. Other P-39s served with Free French and British forces

United Kingdom

P-39N-1 "Saga Boy II" (42-19447)

In 1940, the British Direct Purchase Commission in the US was looking for combat aircraft; they ordered 675 of the export version Bell Model 14 as the "Caribou" on the strength of the company's representations on 13 April 1940. The performance of the Bell P-39 prototype and 13 test aircraft which were able to achieve a speed of 390 mph at altitude was due to the installation of turbo-supercharging. The British armament was 0.50-inch machine guns in the fuselage, and four 0.30-inch machine guns in the wings, the 37 mm gun was replaced by a 20 mm Hispano Suiza.

The British export models were renamed "Airacobra" in 1941. A further 150 were specified for delivery under Lend-lease in 1941 but these were not supplied. The Royal Air Force (RAF) took delivery in mid 1941 and found that actual performance of the non-turbo-supercharged production aircraft differed markedly from what they were expecting[1]. In some areas, the Airacobra was inferior to existing aircraft such as the Hawker Hurricane and Supermarine Spitfire and its performance at altitude suffered drastically. On the other hand it was considered effective for low level fighter and ground attack work. Problems with gun and exhaust flash suppression and compass were fixable.

The need of the USSR was determined to be greater however and Airacobras already in the UK along with the remainder of the first batch being built in the US were sent to the Soviet Air force.

US

The US requisitioned 200 of the next part of the order as the P-400. The P-400 designation came from advertised top speed of 400 mph. After Pearl Harbor, the P-400 was deployed to training units, but some saw combat in the Southwest Pacific including with the Cactus Air Force in the Battle of Guadalcanal.[2] Guns salvaged from P-39s were sometimes fitted to Navy PT boats to increase firepower.[3]

From September to November 1942 pilots of the 57th Fighter Squadron flew P-39s and P-38s from an airfield built on land bulldozed into Kuluk Bay on the barren island of Adak in Alaska's Aleutian Islands. They attacked the Japanese forces which had invaded Attu and Kiska islands in the Aleutians in June 1942. The number one foe that claimed the most lives, however, was not the Japanese but the weather. The low clouds, mist, fog, driving rain, snow and high winds made flying dangerous and lives miserable. The 57th remained in Alaska until November 1942 and then returned to the United States.

Bell P-39 Airacobra in flight firing all weapons at night.

USSR

The most successful use of the P-39 was in the hands of the VVS (Soviet Air Force). The tactical environment of the Eastern Front did not demand the extreme high-altitude operations that the RAF and USAAF employed with their big bombers. The P-39's inherent weakness was its lack of a turbocharger but in the relatively low-altitude operations in the East, this was not as great a handicap. The low-speed, low-altitude turning nature of most air combat on the Russian Front suited the P-39's strengths: sturdy construction, reliable radio gear and adequate firepower. It was common for the Soviet pilots to remove the wing guns and rely only the cannon and nose machine guns as armament. The P-39 was well liked by VVS pilots. The second-highest scoring Allied ace, Aleksandr Pokryshkin, flew the P-39 from late 1942 until the end of the war; his unofficial score in the Airacobra stands at nearly 60 Luftwaffe aircraft. His wingman, Grigori Rechkalov, scored 57 victories with the P-39. This is the highest score ever gained by any pilot with any US-made aircraft. The usual nickname for the Airacobra in the VVS was Kobrusha, "dear little cobra".

Postwar

The Airacobra was raced at the National Air Races in the United States after World War II. Famous versions used for racing included the twin aircraft known as "Cobra I" and "Cobra II," owned jointly between three Bell Aircraft test pilots, Chalmers "Slick" Goodlin, Alvin M. "Tex" Johnston, and Jack Woolams. These craft were extensively modified to use the larger and more powerful P-63 Kingcobra engine and had prototype propeller blades from the Bell factory. "Cobra I" with its pilot, Jack Woolams, was lost in 1946, over the Great Lakes while he was flying from the National Air Races in Cleveland, Ohio back to the factory to get a fresh engine.

The "Cobra II" (Race #84) flown by famed test pilot "Tex" Johnston, beat out P-51 Mustangs and other P-39 racers, which were the favorites, to win the 1946 Thompson Trophy race. Cobra II raced again in the 1947 Thompson Trophy race, finishing 3rd. It raced yet again in the 1948 Thompson trophy race, but was unable to finish owing to engine difficulties. Cobra II did not race again and was destroyed on August 10, 1968 during a test flight prior to a run on the world piston-engine speed record, when owner-pilot Mike Carroll lost control and crashed. Carroll and the highly-modified P-39 perished.

Mira Slovak's "Mr. Mennen" (Race #21) P-39Q Airacobra was a very fast unlimited racer - a late arrival in 1972 kept this little 2000+ hp racer out of the Reno races, and it was never entered again. Its color scheme was all white with "Mennen" green and bronze trim. It is now owned and displayed by the Kalamazoo Air Zoo. The P-39Q (former USAAC serial no. 44-3908/NX40A), is painted as a P-400, "Whistlin' Britches."

In 1942, an P-39 Airacobra crashed in Fiji, but was not found until a local pig farmer discovered the wreck in 2004. The pilot's body was also found and sent to Hawaii for identification. Personal items were recovered at the site. [2]

A number of P-39s are still in existence of which three are still flying. The Commemorative Air Force flies a Bell P-39 Airacobra painted in the markings and colors of the 350th Fighter Group, which consisted of the 345th, 346th and 347th Fighter Squadrons operating P-39s in North Africa and Italy. At one time, the Airacobra was painted in Russian colors and markings. Bell P-39Q-6-BE USAAF, serial no. 42-19993, "Brooklyn Bum– 2nd" is now at the Fighter Collection in Duxford, UK. The Smithsonian's National Air and Space Museum has P-39Q-15BE, serial no. 44-2433 on display.

Keski-Suomen Ilmailumuseo at Tikkakoski, Finland, has one restored P-39Q Airacobra, "White 26", on static display. The aircraft is originally a Soviet lend-lease plane, shot down and captured by Finnish troops in World War Two. It has been restored in the original wartime camouflage and markings.

Popular culture

  • Introduction to the P-39 (1942) [3] Bell wartime training film (38 min) intended for military pilots examining flight techniques, cockpit layout and armament.
  • Flying the P-39 (1943) [4] Bell Training Film No. A.F. - 110 (23 min) demonstrating techniques for piloting the P-39 including aerobatics and strafing.
  • The P-39 Airacobra is featured in the Russian movie Перегон (2006)(Peregon, Transit) [5]dealing with Lend Lease aircraft in transit to Russia.

Variants

P-39Q-5-BE warbird
Bell XFL-1 Airabonita, Navy version
  • XP-39 - first prototype, unarmed
  • YP-39 - service test version, V-1710-37 (E5) 1,090 hp engine, 12 built
  • YP-39A - intended to have a high-altitude V-1710-31 engine (1,150 hp) but delivered as a regular YP-39, one built.
  • XP-39B - streamlined XP-39 based on NACA wind tunnel testing resulting in revised canopy and wheel door shape, oil and radiator intakes moved from right fuselage to wing roots, increased length (by 1 ft 1 in to 29 ft 9 in) and decreased wingspan (by 1 ft 10 in to 34 ft). Turbosupercharger replaced with single-stage geard supercharger, Allison V-1710-37 (E5) engine rated to 13,300 ft.
  • P-39C - first production version, identical to YP-39 except for V-1710-35 1,150 hp engine. Armed with 1x 37 mm cannon, 2x .50 cal and 2x .30 cal machine guns. First aircraft lacked armor and self-sealing fuel tanks.
  • P-39D - 245 lb of additional armor, self-sealing fuel tanks. Armament increased to 1x 37 mm cannon (30 rounds), 2x .50 cal (200 rounds/gun) and 4x .30 cal (1,000 rounds/gun) machine guns. Provisions for a single 250-lb, 325-lb, or 500-lb bomb under the fuselage.
  • P-39D-1 - Lend-Lease version, Hispano 20 mm cannon instead of the 37 mm cannon
  • P-39D-2 - Lend-Lease version, upgraded V-1710-63 (E6) engine with 1,325 hp; restored the 37 mm cannon; provisions for a single 145 US gallon drop tank under the fuselage.
  • Bell Model 14 - export version, ordered by France but not delivered.
  • P-400 Airacobra I - P-39D for Royal Air Force, briefly called Caribou; Hispano 20 mm cannon (60 rounds) instead of the 37 mm cannon. A total of 200 were requisitioned by USAAF after Pearl Harbor; most were used for training, but some saw service in the Southwest Pacific.
  • XP-39E - intended for Continental I-1430-1 engine with 2,100 hp; see Bell XP-76
  • P-39F-1 - Aeroproducts constant speed propeller
  • P-39F-2 - field conversion of P-39F-1 with additional belly armor and cameras in rear fuselage
  • TP-39F - Two-seat training version, built in small numbers.
  • P-39G - intended to be a P-39D-2 with an Aeroproducts propeller. Due to modifications during production no P-39G were actually delivered. Instead, these aircraft were designated P-39K, L, M and N.
  • P-39J - P-39F with V-1710-59 1,100 hp engine with automatic boost control
  • P-39K - P-39D-2 with Aeroproducts propeller and V-1710-63 (E6) 1,325 hp engine; one aircraft designated P-39K-5 and fitted with a V-1710-85 (E19) engine to serve as a P-39N prototype
  • P-39L - P-39K with Curtiss Electric propeller, revised nose gear for reduced drag, provision for underwing rockets.
  • P-39M - 11 ft 1 in Aeroproducts propeller, V-1710-67 (E8) 1,200 hp engine with improved high-altitude performance at the expense of low-altitude performance, ten mph faster than P-39L at 15,000 ft.
  • P-39N - V-1710-85 (E19) 1,200 hp engine; Aeroproducts propeller enlarged from 10 ft 4 in to 11 ft 7 in starting with 167th aircraft. The P-39N-5 had reduced armor.
  • P-39Q - wing-mounted 0.30 cal machineguns replaced with a single 0.50 cal with 300 rounds of ammunition in a pod under each wing. These wing guns were often removed on Soviet aircraft. P-39Q-21 had a four-bladed Aeroproducts propeller. The P-39Q-30 reverted to a three-bladed propeller because the four-bladed unit worsened directional stability.
  • RP-39Q - Two-seat training version, built in small numbers.
  • P-45 - The P-45 was the initial designation of the P-39C or Model 13.
  • F2L - Seven P-39s were supplied to the US Navy to be used as target drones.
  • XFL-1 - One prototype for the US Navy.
  • A-7 - Proposed radio-controlled target drone, never built.

Operators

Specifications (P-39Q Airacobra)

File:050215-F-1234P-062.jpg
Bell P-39Q Airacobra at the National Museum of the United States Air Force.

General characteristics

  • Crew: One

Performance Armament

  • 1x 37 mm M4 cannon firing through the propeller hub at the rate of 140 rpm with 30 rounds of HE ammo.
  • 4 x .50 cal (12.7 mm) machine guns. Rate of fire was 750 rpm x 1 gun in each wing, only 300 rpm each x 2 guns synchronized in the cowl. Ammo: 200 rounds per nose-gun, 300 per wing-pod.
  • Up to 500 lb (230 kg) of bombs externally

References

  1. ^ Mason 1969, p. 5-6.
  2. ^ [1]
  3. ^ A PT boat restored in Portland, Oregon has been fitted with a replica of such a gun.
  • Green, William. Fighters, Vol. 4, (War Planes of the Second World War). London: MacDonald, 1961.
  • Johnsen, Frederick A. Bell P-39/P-63 Airacobra & Kingcobra. St. Paul, Minnesota: Voyageur Press, 1998. ISBN 1-58007-010-8.
  • Loza, Dmitriy. Attack of the Airacobras: Soviet Aces, American P-39s and the Air War Against Germany. Lawrence, Kansas: University Press of Kansas, 2002. ISBN 0-7006-1140-1.
  • Mason, Francis K. Royal Air Force Fighters of World War Two, Volume One. Garden City, NY: Doubleday & Company Inc., 1971.
  • McDowell, Ernest. P-39 Aircobra in action. Carrollton, Texas: Squadron/Signal Publications, 1980. ISBN 0-89747-102-4.

External links

Related content

Related development

Aircraft of comparable role, configuration, and era

Related lists