Bell YFM-1 Airacuda
The Bell YFM-1 Airacuda was an American heavy fighter and interceptor aircraft developed by Bell Aircraft Corporation during the mid-1930s.
Bell YFM-1 Airacuda - American Aircraft & Warplanes - Fighters

Time Period: World War II
Country of Origin: United States
Type: Fighter Aircraft, Interceptor Aircraft
Manufacturer: Bell Aircraft

Bell YFM-1 Airacuda Aircraft Overview

The Bell YFM-1 Airacuda was a prototype fighter aircraft developed by Bell Aircraft Corporation in the late 1930s. It was a unique aircraft with a number of advanced features for its time, but ultimately proved to be unsuccessful and only two prototypes were built.

The Airacuda was a twin-engine, two-seat aircraft with a pusher configuration. It was armed with two 37mm cannon in a dorsal turret and four .30 caliber machine guns in the nose. The aircraft also featured a tricycle landing gear and was powered by two Allison V-1710 liquid-cooled engines.

One of the unique features of the Airacuda was its laminar flow wing design, which was intended to reduce drag and improve performance. The aircraft also featured a complex cooling system, with coolant flowing through the wings and tail surfaces to help dissipate engine heat.

Despite its advanced features, the Airacuda had a number of problems during testing and never entered production. The aircraft was heavy and underpowered, with a relatively low top speed, and its complex systems proved difficult to maintain. In addition, the Airacuda’s complex turret system was difficult to use in combat, and the aircraft’s performance suffered when firing the heavy 37mm cannon.

After the Airacuda project was canceled, the two prototypes were used for a variety of purposes, including as engine testbeds and for aerial photography. One of the aircraft is preserved at the National Museum of the United States Air Force in Dayton, Ohio.

Bell YFM-1 Airacuda Specifications

  • Crew: five (pilot, copilot/navigator, radio operator/gunner, two gunners)
  • Length: 44 ft 10 in (13.67 m)
  • Wingspan: 69 ft 10 in (21.29 m)
  • Height: 13 ft 7 in (4.14 m)
  • Wing area: 684 sq ft (63.5 m2)
  • Airfoil: NACA 23018/NACA 23009 
  • Empty weight: 13,376 lb (6,067 kg)
  • Gross weight: 17,333 lb (7,862 kg)
  • Max takeoff weight: 21,625 lb (9,809 kg)
  • Fuel capacity: 400 US gal (1,500 L)
  • Powerplant: 2 × Allison V-1710-9 liquid-cooled turbosupercharged V-12, 1,090 hp (810 kW) each
  • Propellers: three-bladed.

Bell YFM-1 Airacuda Performance

  • Maximum speed: 277 mph (446 km/h, 241 kn)
  • Cruise speed: 244 mph (393 km/h, 212 kn)
  • Range: 2,600 mi (4,200 km, 2,300 nmi)
  • Service ceiling: 30,500 ft (9,300 m)
  • Rate of climb: 1,480 ft/min (7.5 m/s)

Bell YFM-1 Airacuda Armament

  • Guns: ** 2 × 37 mm (1.46 in) M4 cannons (110 rpg)
    • 2 × .30 in (7.62 mm) M1919 Browning machine guns in front of nacelles
    • 2 × .50 in (12.7 mm) M2 Browning machine guns (600 rpg) in side blisters
  • Bombs: 20 × 30 lb (14 kg) fragmentation bombs in wing bays

Bell YFM-1 Airacuda Image Gallery

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