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Vought VE-10

From Wikipedia, the free encyclopedia
American prototype flying boat
Vought VE-10
Vought VE-10
General information
TypeFlying boat
National originUnited States
ManufacturerVought
StatusDiscontinued
Number built1
History
Manufactured1919
Introduction date1919
First flightAugust 2, 1919

TheVought VE-10 "Bat Boat" was an American biplane flying boat built in 1919 byVought.

Design and development

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Chance M. Vought announced the VE-10 at around the same time as work began on theVE-9. The aircraft had a short, 3-seat hull and was powered by a 90 hpCurtiss OX-5V8 engine.

Operational history

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The VE-10 made its maiden flight on August 2, 1919, with test pilots James A. Taylor, Jr. and Caleb S. Bragg at the controls.[1] Pilots of the aircraft noted that it was well balanced, easy to control, and had performance similar to many land planes of the time.[2] They also noted that it may have been able to perform stunts; an act that was rare for seaplanes at the time.[2] The September 13, 1919 issue ofAircraft Journal called it "one of the most promising commercial airplanes to make its appearance since thearmistice".[1] Despite the large public interest for the VE-10, Vought failed to sell any aircraft.[3]

Vought offered the VE-10 to theUS Navy, and "exhaustive" test flights were made byUS Naval Air Service Commanders McDonald and Griffin, andUS Army Lieutenant Colonel Harald E. Hartney. All three test pilots were pleased with the VE-10's flight characteristics, but as the Navy did not have a use for the aircraft other than unofficial flights, no orders were placed.[1][3] The final disposition of the VE-10 is unknown.[3]

Variants

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VE-10
1 built
VE-15
Militarized derivative of the VE-10.[4] Not built.

Specifications (VE-10)

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Data from[2]

General characteristics

  • Crew: 1
  • Capacity: 2 passengers
  • Length: 27 ft 0 in (8.23 m)
  • Upper wingspan: 36 ft 0 in (10.97 m)
  • Lower wingspan: 28 ft 4.5 in (8.649 m)
  • Height: 10 ft 5 in (3.18 m)
  • Wing area: 300 sq ft (28 m2)
  • Empty weight: 1,330 lb (603 kg)
  • Max takeoff weight: 1,950 lb (885 kg)
  • Powerplant: 1 ×Curtiss OX-5V8 engine, 90 hp (67 kW)
  • Propellers: 2-bladed wooden propeller

Performance

  • Maximum speed: 80 mph (130 km/h, 70 kn)
  • Stall speed: 46 mph (74 km/h, 40 kn)
  • Endurance: 2½ hr[3]
  • Rate of climb: 325 ft/min (1.65 m/s)

See also

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Aircraft of comparable role, configuration, and era

Related lists

References

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  1. ^abcAircraft Journal. Gardner-Moffat Company. 1919.
  2. ^abcAviation and Aeronautical Engineering. Gardner, Moffat Company. 1919.
  3. ^abcdMoran, Gerard (1978).Aeroplanes Vought 1917-1977. Historical Aviation Album. p. 21.ISBN 0-911852-83-2.
  4. ^Millot, Bernard (2004).Les Avions Vought (in French). Lariviere. p. 526.ISBN 2848900601.

External links

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