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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.
Ekranoplan A-90 Orlyonok. A ground-effect vehicle (GEV), also called a wing-in-ground-effect (WIGE or WIG), ground-effect craft/machine (GEM), wingship, flarecraft, surface effect vehicle or ekranoplan (Russian: экранопла́н – "screenglider"), is a vehicle that is able to move over the surface by gaining support from the reactions of the air against the surface of the earth or water.
Overall, South Korea was one of the main customers of the F-4, with 216 delivered, including 60 "D" models, 55 "E" models and 18 RF-4Cs in service in 2000. [61] [63] The F-4 was the ROKAF's primary fighter until the KF-16 began to be introduced in 1994. [64] The 20 F-4D units at Daegu base were retired as of June 16, 2010, as the company took ...
Differences between the CUH-11 and CUH-12 series included a reduction in rated power from 250 W to 230 W, a reduction in weight from 2.8 to 2.5 kg, and physical buttons. [3] [4] [5] The CUH-12xx series are also referred to as the "C chassis" variant of the PS4. [6] In late June 2015, a 1 TB CUH-11 series machine was announced for European/PAL ...
The wing has a 12 in (30 cm) greater span and 5 sq ft (0.46 m 2) greater area and employs a Riblett 30-413.5 airfoil, which gives a 5 to 8 mph (8 to 13 km/h) higher top speed while retaining a low stall speed. The redesigned airframe also uses aluminum fuselage formers, window sills and door sills, replacing the steel formers and sills in the ...
[1] [2] [3] The Glasair II was designed to FAR Part 23 standards and was extensively tested. Its wing has been tested to +10.5g. As indicated by its name, the aircraft is made from fiberglass. Its 23.3 ft (7.1 m) span wing employs a NASA GA(W)-2 airfoil. The wings have an area of 81.3 sq ft (7.55 m 2) and mount flaps.
The Foxtrot was developed as a four-seat version of the Tango 2 and shares many of the two-seater's features. The Foxtrot has a cantilever low-wing, a four-seat enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration. The rear seats have limited visibility. [1] [2] The aircraft is made from composites.
Data from Plane and Pilot. General characteristics Crew: 1 Capacity: 4 passengers Wing area: 135 sq ft (12.5 m 2) Airfoil: NACA 63(2)-215 Empty weight: 1,200 lb (544 kg) Gross weight: 2,400 lb (1,089 kg) Fuel capacity: 50 U.S. gallons (190 L; 42 imp gal) Powerplant: 1 × Lycoming IO-360 horizontally opposed piston, 180 hp (130 kW) Performance Maximum speed: 161 kn (185 mph, 298 km/h) Cruise ...