Engineering:Thomas-Morse XP-13 Viper
| XP-13 | |
|---|---|
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| Thomas-Morse XP-13 | |
| Role | Fighter |
| Manufacturer | Thomas-Morse |
| Designer | B. Douglas Thomas[1] |
| Introduction | June 1929 |
| Primary user | United States Army Air Service |
| Number built | 1[2] |
The XP-13 Viper was a prototype biplane fighter aircraft designed by the United States company Thomas-Morse Aircraft Corporation. The airplane was delivered to the United States Army in 1929, but they did not adopt it.
Design and development
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This aircraft was one of several B. Douglas Thomas designs built in hopes of a production contract from the Army, following the successful Thomas-Morse MB-3 of 1919. Financed by the company, and named the "Viper", it was officially purchased by the Army in June 1929 and designated "XP-13".
The XP-13 fuselage had a corrugated aluminum skin built over a metal frame; the flying surfaces were also metal-framed, but covered with the traditional fabric. While designed to use the 600 hp Curtiss H-1640-1 Chieftain engine, (a novel 12-cylinder two-row air-cooled radial with the rear cylinders directly behind the front cylinders rather than staggered as normal in a two-row radial[3]) for which the XP-13 incorporated a complex system of baffles to direct cooling air over the engine, the engine simply would not stay cool enough, and in September 1930 it was replaced with a Pratt & Whitney SR1340C Wasp of 450 hp. Ironically, the lower-power engine actually resulted in a speed increase of 15 mph, at least partly because of the weight savings.[4]
In the end, the Army decided against production, Thomas-Morse was acquired by Consolidated Aircraft, and the prototype was lost to an inflight fire.
Variants
- XP-13
- Prototype, serial number 29-453 with 600 hp (448 kW) Curtiss H-1640-1 Chieftain hex engine[2]
- XP-13A
- The XP-13 modified with a 525 hp (391 kW) Pratt & Whitney SR-1340-C enclosed in a NACA cowling, along with a revised fin and rudder[5]
- XP-14
- This designation was used for a proposed Curtiss version of the Viper with the Curtiss H-1640-1 Chieftain hex engine
Operators
United States
- United States Army Air Service
Specifications (XP-13 (Chieftain engine))
Data from William Green; Gordon Swanborough (1994). The Complete Book of Fighters: An Illustrated Encyclopedia of Every Fighter Aircraft Built and Flown. Salamander. ISBN 978-0-86101-643-3. https://books.google.com/books?id=zVeXAAAACAAJ.
General characteristics
- Crew: 1
- Length: 23 ft 6 in (7.16 m)
- Wingspan: 28 ft 0 in (8.53 m)
- Height: 8 ft 5 in (2.56 m)
- Wing area: 189 sq ft (17.6 m2)
- Empty weight: 2,262 lb (1,026 kg)
- Gross weight: 3,256 lb (1,477 kg)
- Powerplant: 1 × Curtiss H-1640-1 Chieftain 12-cyliner two-row air-cooled radial engine, 600 hp (448 kW)
Performance
- Maximum speed: 150 kn (172 mph, 277 km/h) (at sea level)
- Cruise speed: 113 kn (130 mph, 209 km/h) [6]
- Range: 168 nmi (193 mi, 312 km) [6]
- Service ceiling: 20,775 ft (6,300 m)
- Rate of climb: 1,700 ft/min (8.6 m/s) [6]
Armament
none
See also
Related lists
- List of fighter aircraft
- List of military aircraft of the United States
References
- Notes
- ↑ The Complete Book of Fighters Editors: William Green & Gordon Swanborough (Barnes & Noble Books New York, 1998, ISBN:0-7607-0904-1)
- ↑ 2.0 2.1 "U.S. Army Aircraft 1908–1946" by James C. Fahey, 1946, 64pp.
- ↑ Gunston 1986, p.46.
- ↑ "U.S. Fighters", by Lloyd S. Jones, (Aero Publishers, Inc. ISBN:0-8168-9200-8, 1975) pp. 46–47
- ↑ "The American Fighter", Enzo Angellucci and Peter Bowers, (Orion Books ISBN:0-517-56588-9), 1987
- ↑ 6.0 6.1 6.2 Dorr and Donald 1990, p.43
- Bibliography
- Dorr, Robert F. and David Donald. Fighters of the United States Air Force. London:Temple, 1990. ISBN:0-600-55094-X.
- Gunston, Bill, World Encyclopedia of Aero Engines. London: Guild Publishing, 1986.
External links
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