Naval Aircraft Factory TS

"F4C" redirects here. For the F-4C jet fighter, see McDonnell Douglas F-4 Phantom II.
TS-1
A TS-1 assigned to the USS Langley (CV-1).
Role Fighter
Manufacturer Naval Aircraft Factory & Curtiss Aeroplane and Motor Company
Designer Bureau of Aeronautics; Rex Buren Beisel[1]
Introduction December 1922
Retired 1929
Status retired
Primary user United States Navy
Number built 46


The Naval Aircraft Factory TS-1 was an early biplane fighter aircraft of the United States Navy, serving from 1922-1929.

Development

While the Vought VE-7s were serving the Navy well in the early 1920s, they were not originally designed as fighters. The Naval Aircraft Factory came up with a simple design driven by a 200 hp (150 kW) Lawrance J-1 air-cooled radial engine. Its boxy fuselage was suspended between the upper and lower wings (essentially having both dorsal and ventral sets of cabane struts), with the center area of the lower wing enlarged to accommodate a fuel tank.[2]

The NAF provided Curtiss with the plans to build the aircraft, and the result, designated TS-1, arrived at Anacostia on May 9, 1922. The TS-1 from Curtiss was delivered with wheels, so the NAF also designed wooden floats to enable their use on vessels other than aircraft carriers. Testing went well, and in late 1922 the Navy ordered 34 planes from Curtiss, with the first arriving on board the USS Langley (CV-1) in December. The NAF built another five themselves, as a test of relative costs, as well as four more used to experiment with water-cooled inline engines.[2]

Two all-metal versions of the aircraft, F4C-1s, were developed by Curtiss. This aircraft made its first flight on September 4, 1924. The wings had tubular spars and stamped duraluminum ribs, the fuselage was constructed of duraluminum tubing in a Warren truss form. Compared to the TS-1, the lower wing was raised to the base of the fuselage. The F4C-1 was armed with two .30 in (7.62 mm) machine guns and was powered by a 200-hp nine-cylinder Wright J-3 radial.

Operational history

In addition to operating from the carrier deck, the TS-1s served for several years in floatplane configuration aboard destroyers, cruisers, and battleships. The aircraft were slung over the side by crane. Squadron VO-1 operated this way from 1922, and VF-1 flew its float-equipped TS-1s from battleships in 1925 and 1926.[3]

The TS-1 was not universally liked by its crews. Positioning of the lower wing below the fuselage resulted in short wheel struts. This, and the wheel's placement close to each other caused considerable problems with ground looping.[4]

Variants

NAF TS-1
five built[3]
Curtiss TS-1
Curtiss TS-1
34 built[3]
NAF TS-2
two built, 240 hp (180 kW) Aeromarine engine[3]
NAF TS-3
two built, 180 hp (130 kW) Wright-Hispano E engine[3]
The first F4C-1 in 1924.
An F4C-1
NAF TR-2
one built, TS-3 modified by changing the airfoil section on the wings for the 1922 Curtiss Marine Trophy race[3]
Curtiss-Hall[5] F4C-1
two built all metal versions for comparison to the original wood and wire construction[3]

Operators

 United States

Survivors

Specifications (TS-1)

Data from Gordon Swanborough, Peter M. Bowers: United States Navy aircraft since 1911. Naval Institute Press, Annapolis 1990 (ISBN 0-87021-792-5), p. 370.

General characteristics

Performance

Armament

1 fixed forward-firing 0.3 in Browning machine gun


References

  1. ↑ Johnson, E.R., United States Naval Aviation, 1919-1941: Aircraft, Airships and Ships Between the Wars; McFarland, 2011; ISBN 078648585X, 9780786485857
  2. 1 2 Lloyd S. Jones, U.S. Naval Fighters (Fallbrook CA: Aero Publishers, 1977, ISBN 0-8168-9254-7), pp. 14-17
  3. 1 2 3 4 5 6 7 "United States Navy Aircraft Since 1911" by Gordon Swanborough & Peter M. Bowers (Naval Institute Press Annapolis, MD, ISBN 0-87021-968-5) 1976, 546 pp.
  4. ↑ Melton USNR, Lt. Comdr. Dick. the Forty Year Hitch. Wyandotte, Michigan: Publishers Consulting Services, 1970
  5. ↑ "The Smithsonian National Air and Space Museum Directory of Airplanes their Designers and Manufacturers" ed. Dana Bell, ISBN 1-85367-490-7, 2002, page 88
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