Curtiss P-40 Warhawk
Country of Origin:
United States | Type: Single seat fighter-bomber
Introduction
The simple expedient of replacing the Curtiss Hawk 75/P-36's radial engine with a supercharged Allison V-1710 V12 created the Curtiss Model 81 P-40 series of fighters. The first XP-40 was a conversion of the 10th production P-36A, flying with its newly installed engine on 14th October 1938. Initially fitted with an underfuselage engine radiator which was subsequently moved to the more familiar lower nose position, the XP-40 impressed the USAAC sufficiently for it to place an order for 524 aircraft worth 12.9 million US dollars, at the time the largest contract issued to an American manufacturer since World War One.
Initial Variants
The initial production model was dubbed simply the P-40 and the first was flown in April 1940 with deliveries beginning two months later. There was no P-40A and the two major USAAC/USAAF production versions were the P-40B with additional wing guns and smoe armour protection, and the P-40C (flown in April 1941) with self sealing fuel tanks and provision for a drop tank. Of the 107 P-40B/Cs in Hawaii at the time of the Pearl Harbour raid, 80 were destroyed. The major user of the early model P-40 was the RAF under the name Tomahawk. Britain took over France's order for 230 aircraft on the latter's capitulation and also acquired large numbers in its own right. They were the Tomahawk I (equivalent to the basic P-40), IIA (P-40B) and IIB (P-40C) for a total of 1,180 aircraft incorporating British calibre (0.303 inch) wing guns.
Series Development
The development in 1940 of a new series of Allison V-1710 engines led to the Curtiss Model 87 Hawk series, beginning with the Model 87A P-40D and E, the first of which flew in May 1941. The engines featured some physical differences resulting in the new Hawks having a revised nose shape with raised propeller thrust line (which in turn allowed shorter main undercarriage legs), modified cockpit lines, a lowered and recontoured fuselage top line and the moving forward of the chin radiator. The new nose necessitated the moving of all gun armament to the wings and this was updated at the same time to 50-calibre weapons.
Major Production
The major production variant of the first series was the Model 87A-1 Kittyhawk IA for Britain and the Commonwealth nations, the first Hawk variant to be supplied under Lend-Lease. These found their way into RAF, RCAF and RAAF service from early 1942, the latter receiving the first of 163 in March 1942 (out of a total of 848 Kittyhawks) at a time when Australa was under threat of invasion by Japan and had no fighters. The Australian Kittyhawks were immediately pressed into action in the country's North and New Guinea.
Merlin Power
The decision to fit an American built Rolls Royce Merlin engine into the P-40 was taken due to the fact that although it was a rugged and tough workhorse, performance was not up to what was expected, and so the decision was to build them with these engines. Packard gained a licence to build the British Merlin 28 (designated V-1650-1 for the US) during late 1940, and it was fitted with a two speed turbocharger. Merlin powered P-40s were designated the P-40F (Hawk 87B by the factory), and the first of then (a P-40D) flew in June 1941. The British designation was Kittyhawk II. The P-40F was distinguishable from previous versions of the type by the removal of the carburretor intake fairing on the top of the engine cowling.
Later Models
Later models of the P-40 were powered by more powerful Allison engines, and were fitted with more armament. The P-40N was the most produced version of the later models, which accounted for almost 40% of the total production. Introduced in early 1943, the P-40N was an attempt to redress the aircraft's basic performance shortcomings which were becoming more marked as time went on. Weight saving was the key to its design with lightened structure, reduced armour, guns and ammunition removed and forward wing tanks eliminated.
Specification
Dimensions
- P-40A/B/C - Wingspan: 11.37 metres (37 feet 3½ inches)
- Length: 9.66 metres (31 feet 8½ inches)
- Height: 3.22 metres (10 feet 7 inches)
- P-40F-5 - Wingspan: 11.38 metres (37 feet 4 inches)
- Length: 10.16 metres (33 feet 4 inches)
- Height: 3.76 metres (12 feet 4 inches)
Powerplant
- P-40A/B/C - one 1,040hp (775kW) Allison V-1710-33 V12 with three bladed propeller
- P-40D/E - one 1,150hp (857kW) Allison V-1710-39 V12 with three bladed propeller
- P-40F/L - one 1,300hp (969kW) Packard Merlin V-1650-1 V12 with three bladed propeller
- P-40K - one 1,325hp (988kW) Allison V-1710-73 V12 with three bladed propeller
- P-40M - one 1,200hp (895kW) Allison V-1710-81 V12 with three bladed propeller
- P-40N - one 1,200hp (895kW) Allison V-1710-81, -99 or -115 V12 with three bladed propeller
Weights
- P-40C - Empty: 2,636kg (5,812lb)
- Normal Loaded: 3,424kg (7,549lb)
- Maximum Loaded: 3,655kg (8,058lb)
- P-40E - Empty: 2,858kg (6,300lb)
- Normal Loaded: 3,810kg (8,400lb)
- Maximum Loaded: 4,128kg (9,100lb)
- P-40F-5 - Empty: 3,175kg (7,000lb)
- Loaded: 3,855kg (8,500lb)
- P-40N-1 - Empty: 2,903kg (6,400lb)
- Loaded: 4,014kg (8,850lb)
- P-40N-20 - Maximum Overload: 5,171kg (11,400lb)
Armament
- P-40A/B/C - two 0.50 inch machine guns in nose and two or four 0.30 inch machine guns in wings
- P-40D - four 0.50 inch machine guns in wings
- P-40E - six 0.50 inch machine guns in wings
- Bomb Load: one 227kg (500lb) bomb under fuselage, or two 45kg (100lb) bombs under wings
- P-40F/L - six 0.50 inch machine guns in wings
- Bomb Load: one 227kg (500lb) bomb under fuselage or two 45kg (100lb) underwing bombs
- P-40K/M - four or six 0.50 inch machine guns in wings
- Bomb Load: one 227kg (500lb) bomb under fuselage or two 45kg (100lb) bombs under wings
- P-40N - up to three 227kg (500lb) bombs
Performance
- P-40C - Maximum Speed: 345mph (555km/h) at 4,572 metres (15,000 feet)
- Cruise Speed: 273mph (439km/h)
- Initial Climb: 820 metres (2,690 feet) per minute
- Service Ceiling: 9,875 metres (32,400 feet)
- Range: 800 miles (1,287 kilometres)
- Maximum Range with Drop Tank: 1,230 miles (1,979 kilometres)
- P-40E - Maximum Speed: 335mph (539km/h) at 1,524 metres (5,000 feet), 362mph (582km/h) at 4,572 metres (15,000 feet)
- Cruise Speed: 207mph (333km/h)
- Initia Climb: 625 metres (2,050 feet) per minute
- Time to 6,096 metres (20,000 feet): 13 minutes
- Service Ceiling: 8,839 metres (29,000 feet)
- Range: 670 miles (1,078 kilometres)
- Range with Drop Tank: 900 miles (1,448 kilometres)
- P-40F-5 - Maximum Speed: 320mph (515km/h) at 1,524 metres (5,000 feet), 364mph (586km/h) at 6,096 metres (20,000 feet)
- Cruise Speed: 208mph (335km/h)
- Initial Climb: 732 metres (2,400 feet) per minute
- Time to 4,572 metres (15,000 feet): 7 minutes 35 seconds
- Range: 600 miles (965 kilometres)
- Maximum Range: 1,500 miles (2,414 kilometres)
- P-40N-1 - Maximum Speed: 313mph (504km/h) at 1,524 metres (5,000 feet), 348mph (560km/h) at 4,572 metres (15,000 feet)
- Cruise Speed: 210mph (338km/h)
- Maximum Climb: 739 metres (2,425 feet) per minute
- Time to 4,572 metres (15,000 feet): 6 minutes 45 seconds
- Service Ceiling: 9,144 metres (30,000 feet)
- Range: 550 miles (885 kilometres)
- Maximum Range: 1,250 miles (2,011 kilometres)
Production
Production of the aircraft totalled 13,738, including:
- 199 P-40
- 131 P-40B
- 193 P-40C
- 140 Tomahawk I
- 110 Tomahawk IIA
- 930 Tomahawk IIB
- 22 P-40D
- 820 P-40E
- 560 Kittyhawk I
- 1,500 Kittyhawk IA
- 1,311 P-40F/Kittyhawk II
- 700 P-40L/Kittyhawk II
- 1,300 P-40K
- 600 P-40M
- 5,216 P-40N
Operators
Australia
Brazil
Canada
Republic of China (Taiwan)
Egypt
Finland
France
Indonesia
Japan
Netherlands
New Zealand
Poland
South Africa
Soviet Union
Turkey
United Kingdom
United States
Three-view Schematic
To view the schematic, click on the image below:

