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Vought V 173

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Top speed
  
222 km/h

Length
  
8.13 m

Manufacturer
  
Developed into
  
Wingspan
  
7.1 m

Engine type
  
Continental O-170

First flight
  
November 23, 1942


Vought v 173 flying pancake


The Vought V-173 "Flying Pancake" was an American experimental test aircraft built as part of the Vought XF5U "Flying Flapjack" United States Navy fighter aircraft program during World War II.

Contents

Vought V-173 Vought V173 Flying Pancake National Air and Space Museum

Both the V-173 and the XF5U featured an unorthodox "all-wing" design consisting of flat, somewhat disk-shaped bodies (hence the name) serving as the lifting surface. Two piston engines buried in the body drove propellers located on the leading edge at the wingtips.

Design and development

Vought V-173 Vought V173 Wikipedia

In the 1930s, Charles H. Zimmerman was a noted aeronautical engineer who advocated the concept of "discoidal" aircraft, the so-called "Zimmer Skimmer" and worked on a variety of projects on his own and with the Vought company. After testing using scale models, including a remotely controlled, electrically powered large-scale model, designated the Vought V-162, the US Navy approached Zimmerman and offered to fund further development. Data and concept documentation was given to the Navy in 1939, with wind tunnel tests on full-scale models being completed in 1940-1941.

Vought V-173 PRESENTATION THE CHANCE VOUGHT V173 FLYING PANCAKE Frontiers

The original prototype, designated the V-173 (Flying Pancake), was built of wood and canvas and featured a conventional, fully symmetrical aerofoil section (NACA 0015). Designed as a "proof-of-concept" prototype, the initial configuration V-173 was built as a lightweight test model powered by two 80 hp (60 kW) Continental A-80 engines turning F4U Corsair propellers. These were replaced by a pair of specially modified 16 ft 6 in three-bladed units. A tall, fixed main undercarriage combined with a small tailwheel gave the aircraft a 22° "nose-high" angle.

Vought V-173 Vought V173 Wikipedia

The disc wing design featured a low aspect ratio that overcame the built-in disadvantages of induced drag created at the wingtips with the large propellers actively cancelling the drag-causing tip vortices. The propellers were arranged to rotate in the opposite direction to the tip vortices, allowing the aircraft to fly with a much smaller wing area. The small wing provided high maneuverability with greater structural strength.

Vought V-173 The Pancake Lives On Flight Journal

In January 1942, BuAer requested a proposal for two prototype aircraft of an experimental version of the V-173, known as the VS-135. The development version, the Vought XF5U-1, was a larger aircraft with all-metal construction, and was almost five times heavier.

Operational history

The first flight of the V-173 was on 23 November 1942 with Vought Chief Test Pilot Boone Guyton at the controls. The aircraft's most significant problem concerned its complicated gearbox that routed power from the engines to its two long propeller shafts. The gearbox produced unacceptable amounts of vibration in ground testing, delaying the aircraft's first test flight for months. Flight testing of the V-173 went on through 1942 and 1943 with 190 flights, resulting in reports of UFOs from surprised Connecticut locals. Charles Lindbergh piloted the V-173 during this time and found it surprisingly easy to handle and exhibiting impressive low-speed capabilities. On one occasion, the V-173 was forced to make an emergency landing on a beach. As the pilot made his final approach, he noticed two bathers directly in his path. The pilot locked the aircraft's brakes on landing, causing the aircraft to flip over onto its back. Remarkably, the airframe proved so strong that neither the plane nor the pilot sustained any significant damage.

The developmental V-173 made its last flight 31 March 1947. In 131.8 hours of flying over 190 flights, Zimmerman's theory of a near-vertical takeoff- and landing-capable fighter had been proven.

Aircraft on display

As of April 2012, after undergoing a long restoration by Vought Aircraft Heritage Foundation volunteers, the V-173 is on loan from the Smithsonian Institution to the Frontiers of Flight Museum in Dallas, Texas.

Specifications (V-173)

General characteristics

  • Crew: One, pilot
  • Length: 26 ft 8 in (8.128 m)
  • Wingspan: 23 ft 4 in (7.1 m)
  • Height: 14 ft 9 in (4.51 m)
  • Wing area: 427 ft2 (44.2 m2)
  • Loaded weight: 2,258 lb (1,024 kg)
  • Powerplant: 2 × Continental A-80 horizontally opposed, four-cylinder engines, 80 hp (60 kW each) each
  • Performance

  • Maximum speed: 138 mph (222 km/h)
  • Rate of climb: to 5,000 ft in 7 min (1,100 m in 5 min)
  • References

    Vought V-173 Wikipedia


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