Comparison of P-40 variants
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Contents |
[edit] Major P-40 variants
The P-40 went through four significant transformations in its military career.
[edit] P-40 / P-40B / P-40C (RAF "Tomahawk Mk I" and "Tomahawk Mk IIA and IIB")
Distinguishing Features: Twin nose guns, smaller engine cowling
Time in Service:
1941-1943
Important Service:
USAAF (1941 - 1942) Pearl Harbor and Philippines AVG (1941-1942) China / Burma RAF / Desert Air Force (1941-1943) North Africa and Syria VVS (1942-1943) Barbarossa and Continuation war
Commentary: This was a very important type for the allies in the early part of the war. Slaughtered mostly on the ground at Pearl Harbor and in the Philippines, it did well with the AVG in China and Burma, and was the most effective fighter available to the RAF in the early months of the Desert War. It was also a small but important part of the Soviet arsenal in 1942, being one of the few types available to them which could take on the Me 109. The earliest version (P-40) had only four guns and lacked armor plate or self sealing tanks, but the British pressed these into service into North Africa anyway as Tomahawk I. The P-40B (Tomahawk IIa) had the some armor, armored windscreen and partially protected fuel tanks, the P-40C (Tomahawk IIb) had a fully protected fuel system and became heavier, reducing speed to under 350 mph. The Soviets reportedly stripped the wing guns from some of their Tomahawks to improve performance.
It's important to note that there were a variety of differences between the British and US variants, (starting with the guns, .303 instead of .30 caliber) so that it's not actually an exact correlation between specific US variants (P-40B etc.) and their rough Commonwealth export equivalents (i.e. 'Tomahawk')
[edit] P-40 D / E / K (RAF "Kittyhawk Mk 1", "Kittyhawk Mk Ia" and "Kittyhawk Mk III")
Distinguishing Features: Deeper engine cowling, ('definitive' P-40 "Look") Six Gun armament, P-40K has expanded tail fin
Time in Service:
1942-1943
Important Service:
USAAF (1942-1943) New Guinea, Guadalcanal, CBI Theater RAAF (1942-1943) Kokoda Trail, Milne Trail, Darwin RNZAF (1942-1943) South Pacific RAAF (1942) Desert War, principle air superiority fighter for early 1942 Soviet / VVS (late 1942-1943)
Commentary: This was the first version armed with six .50 caliber machine guns. More powerful than the P-40B/C in terms of both armor, armament and performance, this was the type which fought as a fighter during the most crucial period in both the Pacific and North African campaigns. The P-40E played a major role in the defense of Australia and New Guinea in 1942, and with the Desert Air Force in intense fighting against the Luftwaffe and Regia Aeronautica also in 1942. The P-40K was the primary type used by the 10th Air Force to establish air superiority in the China / Burma theater, achieving dominance over Japanese Army types in that theater. The P-40E was also an important type for the Soviets.
In the Desert War the arrival of the Kittyhawk led to the early retirement of the Me 109E and it's replacement by the faster and more maneuverable Me 109F. The top scoring RAF squadrons including No's 3 and 112 squadron transitioned from the Tomahawk to the Kittyhawk, scoring many kills against Luftwaffe and Reggia Aeronautica types, helping the Desert Air Force hold on through this tough period.
[edit] P40 F / L (RAF "Kittyhawk Mk II and IIa")
Distinguishing Features: Packard-Merlin engine, no intake on top of engine, some models were lengthened, some had deleted wing guns.
Important Service:
USAAF (1943) Operation Torch, Mediterranean Theater VVS (1943) Free French (1943) Mediterranean Theater
Commentary:
This version fulfilled the longstanding wish of the British to put a Merlin engine in a P-40 (which is what led to the development of the P-51), but it arrived in combat relatively late and ironically, few of this type made it to Commonwealth units. It was however the variant with which the USAAF faced the Luftwaffe and Regia Aeronautica in the Med. The Packard Merlin engine improved performance, but the single stage, two-speed supercharger still limited the effective ceiling to about 20,000 feet. Many P-40F types were lightened in the field by US squadrons to make them 'hot' by removing some armor and wing guns. The P-40L was an official light version nicknamed "Gypsy Rose Lee". Some had four guns some only had two, top speed for this type was 368 mph, climb and acceleration were better as well. This fighter could cope with the Me 109F and G within its effective performance ceiling, it was the variant used by the successful 324th, 325th and 57th fighter groups, and also by the Tuskegee Airmen's 99th FS in Italy for a short time.
P-40F/L variants were supplied to Free French squadrons flying in North Africa.
Some of the later run P-40F/L types were lengthened like the later P-40N, a measure to cope with the increased torque of more powerful engines.
[edit] P-40 M / N (RAF "Kittyhawk Mk III and IV", USAAF "Warhawk")
Distinguishing Features: Modified rear cockpit with expanded view, lengthened fuselage, some models had deleted wing guns
Important Service:
USAAF: (1943-1944) CBI RAF: (1943-1944) Mediterranean Theater RAAF: (1943-1944) South Pacific RNZAF: (1943-1944) South Pacific VVS: (1943)
Commentary:
This version remained in use as an air superiority fighter in the CBI. In other theaters it was principally used as a fighter / bomber. It featured a lengthened fuselage and a more powerful 1300 hp Allison engine but the use of a single speed, single stage supercharger gave the planes just a marginally better effective altitude than a P-40E/K. As with the F/L, there were both 'light' and 'heavy' versions, the lightest 'hot' fighter configuration P-40Ns achieved a top speed of up to 378 Mph. Most P-40M types were actually heavier and made just 345 Mph. Later run P-40Ns were made with a smaller engine, specifically for training or fighter-bomber missions.
This table compares the specifications of one early- and one late-model P-40 variant.
P-40E | P-40N | |
General characteristics | ||
---|---|---|
Crew | One | One |
Length | 31 ft 8 in (9.66 m) | 33 ft 4 in (10.16 m) |
Wingspan | 37 ft 4 in (11.38 m) | 37 ft 4 in (11.38 m) |
Height | 12 ft 4 in (3.76 m) | 12 ft 4 in (3.76 m) |
Wing area | 235.94 ft² (21.92 m²) | 235.94 ft² (21.92 m²) |
Empty weight | 6,350 lb (2,880 kg) | 6,405 lb (2,905 kg) |
Loaded weight | 8,280 lb (3,760 kg) | 7,730 lb (3,505 kg) |
Maximum gross takeoff weight | 8,810 lb (4,000 kg) | 8,860 lb (4,020 kg) |
Powerplant | 1x Allison V-1710-39, 1,150 hp (860 kW) |
|
Performance | ||
Maximum speed | 360 mph (580 km/h) | 378 mph (608 km/h) at 5,000 m (16,400 ft)(light version) |
Cruise speed | 270 mph (435 km/h) | 280 mph (455 km/h) |
Range | 650 mi (1,050 km) | 745 mi (1,200 km) |
Service ceiling | 29,000 ft (8,840 m) | 31,000 ft (9,450 m) |
Climb rate | 2,100 ft/min (10.7 m/s) | 2,240 ft/min (11.4 m/s) |
Wing loading | 35.1 lb/ft² (171.5 kg/m²) | 32.8 lb/ft² (159.9 kg/m²) |
Power/mass | 0.14 hp/lb (230 W/kg) | 0.16 hp/lb (260 W/kg) |
Armament | ||
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