Grumman XF4F-2 BuNo 0383 2

Grumman XF4F-2 BuNo 0383 2

XF4F-2 0383 2

The Grumman XF4F-2 Wildcat (Model G-18) was an early iteration of what would become one of the U.S. Navy’s most iconic fighters during World War II. This prototype represented Grumman’s effort to enter the monoplane fighter arena, as biplane designs were becoming increasingly outdated. Below are the key details and historical context of the XF4F-2:

Key Specifications and Features of the Grumman XF4F-2 Wildcat:

  1. Development and Purpose:

    • The XF4F-2 was Grumman’s second attempt at designing a monoplane fighter for the U.S. Navy after the initial XF4F-1 biplane design was deemed obsolete even before it flew.
    • Development began on August 28, 1936, with the aim of creating a fighter that could compete with other designs like the Brewster XF2A-1 Buffalo.
  2. First Flight:

    • The XF4F-2 made its first flight on September 2, 1937, with test pilot Robert L. Hall at the controls. Hall was notable for his earlier work on the Gee Bee Model Z, a famous racing aircraft.
  3. Physical Characteristics:

    • Wingspan: 34 feet
    • Length: 26 feet 5 inches
    • Height: 11 feet 11 inches
    • Wing Area: 232 square feet
  4. Powerplant and Propulsion:

    • Powered by a Pratt & Whitney R-1830-66 Twin Wasp radial engine, a 14-cylinder, twin-row, air-cooled engine.
    • The engine produced 1,050 horsepower at takeoff and 900 horsepower at 12,000 feet, using a single-stage/single-speed supercharger.
    • The aircraft was equipped with a Hamilton Standard 3-blade constant-speed propeller with a 10-foot diameter.
  5. Armament:

    • The XF4F-2 was armed with two .50 caliber Browning machine guns mounted in the nose.
    • There were provisions to add two more machine guns in the wings, as well as to carry two 100-pound bombs on wing-mounted racks.
  6. Weight and Performance:

    • Empty Weight: 4,035 pounds
    • Gross Weight: 5,386 pounds
    • Maximum Speed: 290 miles per hour at 10,000 feet
    • Normal Range: 740 miles
    • Initial Climb Rate: 2,650 feet per minute
    • Service Ceiling: 27,400 feet
  7. Competitive Context:

    • The XF4F-2 was competing against the Brewster XF2A-1 Buffalo, which was more advanced in some aspects.
    • Despite being innovative, the XF4F-2’s performance did not initially match that of the Buffalo, leading to a return to the factory for modifications.
  8. Legacy and Outcome:

    • The modifications made to the XF4F-2 led to the development of the subsequent XF4F-3, which became the basis for the production F4F Wildcats that would see extensive service during World War II.
    • Although the XF4F-2 did not win the initial competition, the lessons learned from its development were critical in refining the design that would later become one of the U.S. Navy’s primary carrier-based fighters.

The Grumman XF4F-2 was an important step in the evolution of naval aviation, representing Grumman’s successful transition from biplanes to monoplanes. Though it fell short in its initial performance evaluations, the design adjustments and improvements it prompted led directly to the creation of the XF4F-3 and the highly successful F4F Wildcat series, which played a key role in the Pacific Theater during World War II.


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Link to full-size photo:
Grumman XF4F-2 BuNo 0383 2

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