|Role||motor glider transport|
|Manufacturer||Kharkovskii Aviatsionni Institut|
|Designer||Alexandr Alekseyevich Lazerev|
|First flight||14 September 1936|
Design and development
Alexandr Alekseyevich Lazerev, who led the Kharkiv KhAI-3 Avianvito design team, already knew some of the problems posed by tailless aircraft. He was on the team which designed the almost uncontrollable KhAI-4 two years before (the Institute's designs did not always appear in their numerical order). That aircraft made only three flights before being grounded as dangerous.
It was a tailless aircraft with a broad-chord wing and with a tractor engine, fin and rudder all on the centreline. Though there were initial thoughts of mounting the KhAI-3's Shvetsov M-11 five cylinder radial engine on a pylon over the wing, it was finally placed ahead of the leading edge on steel tubes from the front wing spar and fed from four tanks in the central wing. There was a long, six seat cabin on either side of the centreline with the pilot in the forward portside seat. The large, triangular fin mounted a broad, round-topped rudder.
Its central wing panel was rectangular in plan, with a steel tube structure including four spars and dural skinning. It had a chord of 5.0 m (16 ft 5 in) and a chord/thickness ratio of 14%. The outer panels, 82% of the span, were all-wood structures with dihedral and sweep on the leading edge only, giving an overall sweep of 16° at quarter-chord;. They decreased in thickness outwards from 14% to 7%, with 8° washout. Each wing carried three control surfaces. Near each tip, close behind and parallel to the leading edge there was a large, rectangular plan interceptor. These were operated differentially by pedals which also controlled the rudder and were used to make flat turns. Inboard of the interceptors, each outer panel trailing edge carried two broad-chord control surfaces that acted as both ailerons and elevators.
The Kharkiv KhAI-3 had a fixed, tailwheel undercarriage. Its forward-mounted engine and propeller allowed a short tailwheel to provide a ground angle of attack of 15°, avoiding one of the problems encountered with the KhAI-4.
The first flight was made on 14 September 1936. On this occasion the front seats of both cabins were equipped with dual controls; the pilots were V. A. Borodin and E. I. Schwartz. During this and subsequent flights, controlled turns proved difficult however the various control surfaces were combined. A long development programme yielded significant improvements.
- Crew: one
- Capacity: eleven passengers
- Length: 6.8 m (22 ft 4 in)
- Wingspan: 22.4 m (73 ft 6 in)
- Wing area: 78.6 m2 (846 sq ft)
- Aspect ratio: 6.4
- Airfoil: V-106, thinning outwards from 14% to 7%
- Empty weight: 1,440 kg (3,175 lb)
- Gross weight: 2,200 kg (4,850 lb)
- Powerplant: 1 × Shvetsov M-11 5-cylinder air-cooled radial, 93 kW (125 hp) . Sub-type not known so power uncertain.
- Maximum speed: 135 km/h (84 mph, 73 kn)
- Cruise speed: 115 km/h (71 mph, 62 kn)
- Range: 850 km (530 mi, 460 nmi)
- Service ceiling: 2,000 m (6,600 ft)
- Time to altitude: 25 min to 1,000 m (3,300 ft)
- take-off distance: 210 m (690 ft)
- landing speed: 60 km/h (37 mph; 32 kn)
- Gunston, Bill (1995). The Osprey Encyclopedia of Russian Aircraft 1875-1995. London: Osprey (Reed Consumer Books Ltd). p. 148-9. ISBN 1 85532 405 9.