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TAF VIII-2, four-seater Tandem Airfoil Flairboat Typ Jörg II, built in 1983. Following the F&E and test period, Dipl. Ing. Günther Jörg was awarded with the "Phillip Morris Scientific Award" for the Transportation System for the future. Another TAF VIII-2, built in 1994 was given to a Japanese private citizen.
TAF VII-5: Second manned tandem-airfoil Flairboat, 2 seater made of wood; TAF VIII-1: 2-seater tandem-airfoil flairboat built of glass-reinforced plastic (GRP) and aluminium. A small serie of 6 Flairboats had been produced by former Botec Company; TAF VIII-2: 4-seater tandem-airfoil Flairboat built of full aluminium (2 units) and built of GRP ...
An extensively modified version of the UB-14B design was built under licence in the United Kingdom by Cunliffe-Owen Aircraft, powered by two Bristol Perseus XIVC radials as the Cunliffe-Owen OA-1 Clyde Clipper. [2] The UB-14B was to have been built by Scottish Aviation, but with more streamlined inline engines.
Its 32.00 ft (9.8 m) span wing employs a USA 35B airfoil, mounts flaps and has a wing area of 168.00 sq ft (15.608 m 2). The standard conversion installs a 230 hp (172 kW) Ford V6 powerplant, driving a fixed pitch propeller, although engines of up to 300 hp (224 kW) can be employed.
Its 24.00 ft (7.3 m) span wing employs a NACA 63A015/0012 airfoil and has a wing area of 150.0 sq ft (13.94 m 2). The cockpit width is 29 in (74 cm). The acceptable power range is 180 to 300 hp (134 to 224 kW) and the standard engine used is the 300 hp (224 kW) Lycoming IO-540 powerplant. With that engine the aircraft has a cruise speed of 202 ...
Data from Plane & Pilot and Pilot Friend General characteristics Crew: one Capacity: one passenger Length: 20 ft 10 in (6.35 m) Wingspan: 22 ft 10 in (6.96 m) Height: 5 ft 10.75 in (1.7971 m) Wing area: 150 sq ft (14 m 2) Airfoil: Symmetrical Sorrell design Empty weight: 1,236 lb (561 kg) Gross weight: 1,911 lb (867 kg) utility1 category, 1690 lbs (766 kg) aerobatic Fuel capacity: 227 lbs ...
The new wing and airfoil, and the use of a four-bladed propeller, acted to eliminate the high frequency vibrations that had plagued the Typhoon. [10] The design team also chose to use the new Mark IV version of the Napier Sabre H-block 24 cylinder engine for the Tempest, drawings of which had become available to Hawker in early 1941.
Data from Aircraft Spruce General characteristics Capacity: 2 Length: 20 ft 7 in (6.27 m) Wingspan: 24 ft (7.3 m) Height: 7 ft 3 in (2.21 m) Wing area: 165 sq ft (15.3 m 2) Airfoil: M6 Empty weight: 1,000 lb (454 kg) Gross weight: 1,704 lb (773 kg) Fuel capacity: 28 Fuse 15 Wing Powerplant: 1 × Lycoming O-360, 180 hp (130 kW) Performance Maximum speed: 160 kn (180 mph, 290 km/h) Cruise speed ...