|I-14 / ANT-31|
|National origin||Soviet Union|
|First flight||27 May 1933|
|Primary user||Soviet Air Force|
The Tupolev I-14 (also designated ANT-31) was a Soviet fighter aircraft of the 1930s. It was a single-engined, single-seater monoplane with a retractable undercarriage and designed to carry a heavy armament, and as such was one of the most advanced fighters of its time. It was ordered into production, but this was cancelled after only a small number had been built, the competing Polikarpov I-16 being preferred.
Development and design
In 1932, the Soviet Air Force developed a requirement for a high-speed monoplane fighter to serve alongside agile but slower biplane fighters. In order to meet this requirement, the Tupolev design bureau assigned a team led by Pavel Sukhoi. Sukhoi's team came up with the ANT-31, a low-winged monoplane with an unbraced cantilever wing, retractable undercarriage, an enclosed cockpit and a heavy cannon armament. As such, it was one of the most advanced fighters in the world.
The aircraft had a metal monocoque fuselage, while the wings were of corrugated metal construction. The mainwheels of the conventional landing gear retracted backwards into the wing, being operated by cables driven by a handwheel turned by the pilot. The first prototype was powered by an imported 433 kW (580 hp) Bristol Mercury radial engine enclosed by a NACA cowling and driving a two-bladed wooden propeller. It was armed with a single PV-1 machine gun, with provision for two Kurchevsky APK-37 recoilless autocannon under the wing.
The ANT-31, given the air-force designation I-14 (Istrebitel – fighter), made its maiden flight on 27 May 1933. It proved agile but difficult to handle, and with the supercharged Mercury was underpowered, particularly at low altitude. It was therefore decided to build a second prototype, the I-14bis (also known as the ANT-31bis and the I-142 with a more powerful (531 kW (712 kp) Wright Cyclone engine, also imported, an uncorrugated wing and a new undercarriage. The I-14bis demonstrated excellent performance, although handling was still tricky, and an order was placed for production of 55 aircraft, to be powered by the Shvetsov M-25, a licensed version of the Cyclone, and an armament of two 45 mm (1.8 in) Kurchevsky APK-11 recoilless cannons and two ShKAS machine guns.
Deliveries began from the GAZ-125 factory at Irkutsk, Siberia in November 1936. The aircraft's armament had changed to a single ShKAS machine gun and a 20 mm ShVAK cannon as Kurchevsky's recoilless guns had fallen out of favour (with Kurchevsky himself soon to be arrested). By this time, the rival Polikarpov I-16 fighter was well established in production and service, and production of the I-14 was stopped after 18 had been built, the type soon being phased out of service.
Specifications (production I-14)
Data from Tupolev: The Man and His Aircraft
- Crew: 1
- Length: 6.11 m (20 ft 1 in)
- Wingspan: 11.25 m (36 ft 11 in)
- Height: 3.14 m (10 ft 4 in)
- Wing area: 16.8 m2 (181 sq ft)
- Empty weight: 1,170 kg (2,579 lb)
- Gross weight: 1,540 kg (3,395 lb) 
- Powerplant: 1 × Shvetsov M-25 9-cylinder air-cooled radial engine, 521.8 kW (699.7 hp)
- Maximum speed: 449 km/h (279 mph; 242 kn)
- Range: 1,050 km (652 mi; 567 nmi)
- Service ceiling: 9,430 m (30,938 ft)
- Time to altitude: 6.5 min to 5,000 m (16,400 ft)
- Aircraft of comparable role, configuration and era
- Gunston 1995, p.301.
- Gunston 1995, p.401.
- Gunston 1995, pp. 401–402.
- Duffy and Kandalov 1996, p.75.
- Gunston 1995, p.402.
- Gunston 1995, p.XXXII.
- Williams and Gustin 2003, p.309.
- Gunston 1995, p.XIV.
- Duffy and Kandalov 1996, p.209.
|Wikimedia Commons has media related to Tupolev I-14.|
- Duffy, Paul and Andrei Kandalov. Tupolev,: The Man and His Aircraft. Shrewsbury, UK: Airlife Publishing, 1996. ISBN 1-85310-728-X.
- Gunston, Bill. The Osprey Encyclopedia of Russian Aircraft 1875–1995. London:Osprey, 1995. ISBN 1-85532-405-9.
- Williams, Anthony G. and Emmanuel Gustin.Flying Guns: World War II. Shrewsbury, UK: Airlife Publishing, 2003. ISBN 1-84037-227-3.