Chance-Vought V173 Fighter

This 2m dia flying saucer is in actual fact a quarter scale Chance-Vought V173 experimental fighter which dates back to the 1940`s and was being built by Hugh Grant.

Hugh`s model is constructed with 6mm depron ribs, braced and spaced with 1/2 sq spruce spars, all hidden from view under yellow Oracover film. A huge 5 series, 500kv outrunner motor and 4s 4400 mah Lipo in each engine pod. Nearly complete, a maiden flight is expected this summer!

But what about the real life history of this weird looking creature.

In the 1930s, Charles Zimmerman was a noted aeronautical engineer who advocated the concept of "discoidal" aircraft, the so-called "Zimmer's Skimmers" 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.

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.

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.

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.

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 "flying saucers" (unlikely usage, because the term was coined on June 24, 1947 by Kenneth Arnold) 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. The V-173 is now part of the Smithsonian collection at the Paul E. Garber Preservation, Restoration, and Storage Facility in Silver Hill, Maryland. It is currently at the Vought Aircraft plant in Grand Prairie, Texas being restored to go back on display. As of April 2012 it is on loan to the Frontiers of Flight Museum in Dallas, Texas.

General characteristics

Crew: One, pilot

Length: 26 ft 8 in (4.51 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 inline engines, 80 hp (60 kW each) each


Maximum speed: 138 mph (222 km/h)

Rate of climb: to 5,000 ft in 7 min (1,100 m in 5 min)

(Info from Wikipedia)