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P-40

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The Curtiss P-40 Warhawk is an American single-engined, single-seat, all-metal fighter and ground-attack aircraft that first flew in 1938. The P-40 design was a modification of the previous Curtiss P-36 Hawk which reduced development time and enabled a rapid entry into production and operational service. The Warhawk was used by most Allied powers during World War II, and remained in frontline service until the end of the war. It was the third most-produced American fighter of World War II, after the P-51 and P-47; by November 1944, when production of the P-40 ceased, 13,738 had been built,[3] all at Curtiss-Wright Corporation's main production facilities at Buffalo, New York. P-40 Warhawk was the name the United States Army Air Corps gave the plane, and after June 1941, the USAAF adopted the name for all models, making it the official name in the U.S. for all P-40s. The British Commonwealth and Soviet air forces used the name Tomahawk for models equivalent to the original P-40, P-40B, and P-40C, and the name Kittyhawk for models equivalent to the P-40D and all later variants.P-40s first saw combat with the British Commonwealth squadrons of the Desert Air Force in the Middle East and North African campaigns, during June 1941.[4][5] No. 112 Squadron Royal Air Force, was among the first to operate Tomahawks in North Africa and the unit was the first Allied military aviation unit to feature the "shark mouth" logo,[6][7] copying similar markings on some Luftwaffe Messerschmitt Bf 110 twin-engine fighters.[6] [N 1]The P-40's lack of a two-speed supercharger made it inferior to Luftwaffe fighters such as the Messerschmitt Bf 109 or the Focke-Wulf Fw 190 in high-altitude combat and it was rarely used in operations in Northwest Europe. However, between 1941 and 1944, the P-40 played a critical role with Allied air forces in three major theaters: North Africa, the Southwest Pacific, and China. It also had a significant role in the Middle East, Southeast Asia, Eastern Europe,

General Characteristics

  • Created On iOS
  • Wingspan 37.5ft (11.4m)
  • Length 33.0ft (10.1m)
  • Height 13.2ft (4.0m)
  • Empty Weight 5,573lbs (2,528kg)
  • Loaded Weight 8,876lbs (4,026kg)

Performance

  • Horse Power/Weight Ratio 2147483.648
  • Wing Loading 31.0lbs/ft2 (151.4kg/m2)
  • Wing Area 286.2ft2 (26.6m2)
  • Drag Points 2769

Parts

  • Number of Parts 91
  • Control Surfaces 6
  • Performance Cost 570