|First flight||23 November 1942|
|Retired||15 March 1947|
|Developed into||Vought XF5U|
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 developmentEdit
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.
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. The empennage consisted of two vertical fins with rudders, two conventional horizontal stabilizers, and two large elevator/trim surfaces on either side of centerline on the trailing edge of the wing planform.
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. Although a prototype was constructed, it was never flown, as Navy priorities had changed in the meantime.
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 displayEdit
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.
- 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
Aircraft of comparable role, configuration, and era
- Chant 1984, p. 53.
- Winchester X-Planes 2005, p. 223.
- Pearson 2002, p. 50.
- Schoeni 1975, p. 568.
- "Vought V-173 "Flying Pancake"". National Air and Space Museum, Smithsonian Institution. 1998. Retrieved 27 September 2020.
- Winchester Concept Planes 2005, p. 247.
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- Ginter 1992, p. 11.
- Guyton 1991, p. 29.
- "Chance Vought V-173 "Flying Pancake" | Frontiers of Flight Museum". Flightmuseum.com. 23 November 1942. Archived from the original on 26 November 2013. Retrieved 29 May 2013.
- "V-173 Flying Pancake". Vought Heritage. Retrieved 27 December 2016.
- Lee, Russell (20 March 2012). "Vought Aircraft Heritage Foundation Retirees Finish Vought V-173 "Flying Pancake" Following 8-Year Restoration Effort". Smithsonian National Air and Space Museum. Retrieved 2 March 2017.
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Media related to Vought V-173 at Wikimedia Commons