THK-11
A replica THK-11 on display at the Ankara Türk Hava Kurumu Müzesi - (Ankara Turkish Aeronautical Museum)
Role
Cabin monoplane Type of aircraft
National origin
Turkey
Manufacturer
Türk Hava Kurumu (THK - Turkish Aeronautical Association)
First flight
1947
Status
Abandoned
Number built
1
The THK 11 was a 1940s prototype Turkish four-seat monoplane , designed by Stanisław Rogalski and built by Türk Hava Kurumu (THK - Turkish Aeronautical Association).[ 1] [ 2]
Design and development
The THK-11 was a high-wing twin-boom cantilever cabin monoplane with a 135 hp (101 kW) de Havilland Gipsy Major piston engine driving a pusher propeller.[ 1] It has a fixed nose-wheel landing gear[ 2] and was first flown in 1947.
Specifications
Data from Jane's All The World's Aircraft 1951–52,[ 3] Jane's All The World's Aircraft 1949–50[ 4]
General characteristics
Crew: 2
Capacity: 1 passenger
Length: 8.44 m (27 ft 8 in)
Wingspan: 11.80 m (38 ft 9 in)
Height: 2.59 m (8 ft 6 in)
Wing area: 18.7 m2 (201 sq ft)
Empty weight: 828 kg (1,825 lb)
Gross weight: 1,150 kg (2,535 lb)
Powerplant: 1 × de Havilland Gipsy Major four-cylinder air-cooled inverted in-line engine , 101 kW (135 hp)
Propellers: 2-bladed fixed-pitch pusher propeller
Performance
Maximum speed: 201 km/h (125 mph, 109 kn)
Cruise speed: 164 km/h (102 mph, 89 kn)
Landing speed: 80 km/h (50 mph; 43 kn)
Range: 800 km (500 mi, 430 nmi) in still air
Service ceiling: 3,500 m (11,500 ft)
Rate of climb: 3.5 m/s (690 ft/min)
Wing loading: 61.5 kg/m2 (12.6 lb/sq ft)
Power/mass : 11.4 kg/kW (18.7 lb/hp)
See also
Aircraft of comparable role, configuration, and era
References
^ a b "Progress in Turkey" . Flight . Vol. LVI, no. 2127. 29 September 1949. p. 442.
^ a b The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985) . Orbis Publishing. p. 2996.
^ Bridgeman, Leonard (1951). Jane's All The World's Aircraft 1951–52 . London: Sampson Low, Marston & Company, Ltd. p. 191c.
^ Bridgeman, Leonard (1949). Jane's All The World's Aircraft 1949-50 . London: Sampson Low, Marston & Company, Ltd. pp. 183c – 184c .