Engineering:Naval Aircraft Factory TS

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TS-1
NAF-Curtiss TS-1 in flight in the 1920s.jpg
A TS-1 assigned to USS Langley
Role Naval 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 to 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 aircraft carrier USS Langley 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 or launched from capital ship catapults. 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 wheels' 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
All metal versions for comparison to the original wood and wire construction; two built.[3]

Operators

 United States
  • United States Navy
    • VO-1 (Spotting or Observation Plane Squadron) 1922-?
    • VF-1 (Fighting Squadron) 1925-1926

Surviving aircraft

  • A6446 – TS-2/3 owned by the National Air and Space Museum in Washington, D.C.[6] It was previously on display at the National Naval Aviation Museum in Pensacola, Florida.[7]

Specifications (TS-1 landplane)

Data from Curtiss Aircraft 1907–1947,[8] United States Navy aircraft since 1911[9]

General characteristics

  • Crew: 1
  • Length: 22 ft 1.375 in (6.74053 m)
  • Wingspan: 25 ft 0.3125 in (7.627938 m)
  • Height: 8 ft 11.9375 in (2.741613 m)
  • Wing area: 227.8 sq ft (21.16 m2)
  • Airfoil: USA 27[10]
  • Empty weight: 1,239 lb (562 kg)
  • Gross weight: 1,927.5 lb (874 kg)
  • Powerplant: 1 × Lawrance J-1 9-cylinder air-cooled radial piston engine, 200 hp (150 kW)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 131 mph (211 km/h, 114 kn)
  • Cruise speed: 104.8 mph (168.7 km/h, 91.1 kn)
  • Range: 468 mi (753 km, 407 nmi)
  • Service ceiling: 14,400 ft (4,400 m)
  • Rate of climb: 1,200 ft/min (6.1 m/s)

Armament

References

  1. ↑ Johnson, E.R., United States Naval Aviation, 1919-1941: Aircraft, Airships and Ships Between the Wars; McFarland, 2011; ISBN:078648585X, 9780786485857
  2. ↑ 2.0 2.1 Lloyd S. Jones, U.S. Naval Fighters (Fallbrook CA: Aero Publishers, 1977, ISBN:0-8168-9254-7), pp. 14-17
  3. ↑ 3.0 3.1 3.2 3.3 3.4 3.5 3.6 "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
  6. ↑ "Curtiss (NAF) TS-2/3". Smithsonian Institution. http://airandspace.si.edu/collection-objects/curtiss-naf-ts-23. 
  7. ↑ "Curtiss TS.1 SN: A6446". http://www.aero-web.org/museums/fl/nmna/a6446.htm. 
  8. ↑ Bowers, Peter M. (1979). Curtiss aircraft, 1907-1947. London: Putnam. pp. 184–186. ISBN 0370100298. 
  9. ↑ Swanborough, Gordon; Bowers, Peter M. (1990). United States Navy aircraft since 1911. Annapolis: Naval Institute Press. pp. 368–370. ISBN 0-87021-792-5. 
  10. ↑ Lednicer, David. "The Incomplete Guide to Airfoil Usage". https://m-selig.ae.illinois.edu/ads/aircraft.html. 
  • Melton USNR, Lt. Comdr. Dick. the Forty Year Hitch. Wyandotte, Michigan: Publishers Consulting Services, 1970

External links

  • Curtiss TS-1 SN: A6446 on display at the National Museum of Naval Aviation [1]
  • Curtiss TS-1 SN: A6315 photograph in the National Museum of Naval Aviation collection [2]



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