Tairov Ta-3
Ta-3 | |
---|---|
Role | |
National origin | Soviet Union |
Manufacturer | OKO (Kiev) |
Design group | Vsevolod Konstantinovich Tairov (ru) |
First flight | 31 December 1939 (OKO-6) |
Number built | 4 |
The Tairov Ta-3 was a twin-engined single-seat
Development
Tairov designed and built the OKO-6 to a
.The aircraft was a single-seat monoplane of mixed construction; with wing spars of 30KhGSA (30ХГСА) steel,
First flown by Yu. K. Stankevich on 31 December 1939, the first aircraft was also tested by LII until the summer of 1940 when one of the engines threw a connecting-rod. The directional stability was found to be unsatisfactory so the second prototype (OKO-6bis) was built with a much longer rear fuselage, twin fins on the tips of a longer span tailplane as well as more powerful engines with LH rotation.
The third prototype was initially called OKO-6bis, changed to Ta-3, was flown by Stankevich in May 1941 with M-89 engines, one AM-37 37mm cannon and two ShVAK 20mm cannons. The fourth airframe which was to be the Ta-3bis with M-82 engines was abandoned due to the
Variants
- OKO-6 – initial prototype with 950 / 1,000 hp (710 / 750 kW) ShVAKcannon in the forward fuselage.
- OKO-6bis – second prototype with lengthened fuselage, twin fins and M-88R engines. Armament:- 2 x 7.62mm ShKASmachine-guns and 4 x 20mm ShVAK cannon in the forward fuselage.
- Ta-3 – third prototype renamed from OKO-6bis, with M-89 engines and increased span wings. Armament:- 1x 37mm AM-37 cannon and 2 x 20mm ShVAK cannon in the forward fuselage.
- Ta-3bis – uncompleted fourth prototype, with 1,250 hp (930 kW) Shvetsov M-82engines, abandoned with the German invasion of Ukraine. Armament:- 1x 37mm AM-37 cannon and 2 x 20mm ShVAK cannon in the forward fuselage.
Specifications (Ta-3)
Data from Gunston, Bill. "Encyclopaedia of Russian Aircraft 1875-1995". London:Osprey. 1995.
General characteristics
- Crew: one
- Length: 9.827 m (32 ft 2.87 in)
- Wingspan: 12.658 m (41 ft 6.37 in)
- Wing area: 26.9 m2 (290 sq ft)
- Empty weight: 4,500 kg (9,920 lb)
- Gross weight: 6,626 kg (14,607.8 lb)
- Powerplant: 2 × Tumansky M-88R 14-cylinder radial engine , 745.7 kW (1,000 hp) each
Performance
- Maximum speed: 595 km/h (369.7 mph, 321.3 kn)
- Range: 1,060 km (660 mi, 570 nmi)
- Service ceiling: 11,000 m (36,089 ft)
- Rate of climb: 5.55 m/s (1,093.6 ft/min)
Armament
- 1 x 37mm AM-37 cannon
- 2 x 20mm ShVAKcannon
See also
Aircraft of comparable role, configuration, and era
- Focke-Wulf Fw 187
- Fokker D.XXIII
- Gloster F.9/37
- Grumman F5F Skyrocket
- Grushin Gr-1
- IMAM Ro.57
- Kawasaki Ki-45 II
- Lockheed P-38 Lightning
- Westland Whirlwind
References
- Gunston, Bill. “The Osprey Encyclopaedia of Russian Aircraft 1875–1995”. London, Osprey. 1995. ISBN 1-85532-405-9