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MT-Propeller
MT-Propeller Entwicklung GmbH, founded in 1980 by Gerd Muehlbauer, is a manufacturer of composite propellers for single and twin engine aircraft, airships, wind tunnels and other special applications.Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook'', page 84. BAI Communications. The company headquarters is located at Straubing Wallmuhle Airport in Bavaria, Germany. History In 2010 the company developed a special propeller design for restorations of the North American F-82 Twin Mustang The North American F-82 Twin Mustang is the last American piston-engined fighter ordered into production by the United States Air Force. Based on the North American P-51 Mustang, the F-82 was originally designed as a long-range escort fighter .... Applications Factory installed Installed under an STC Installed on unmanned combat aerial vehicle (UCAV) See also * List of aircraft propeller manufacturers References External links *{{Official website, http://www. ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Diamond DA40
The Diamond DA40 Diamond Star is an Austrian four-seat, single-engine, light aircraft constructed from composite materials. Built in both Austria and Canada, it was developed as a four-seat version of the earlier DA20 by Diamond Aircraft Industries. By the end of December 2020, 2,200 DA40s had been delivered, including 500 NG models. Development Based on the success of the earlier DV20/DA20 two-seat aircraft, the company designed a four-seat variant, the DA40 Diamond Star. The Rotax 914-powered prototype DA40-V1, registered OE-VPC, first flew on 5 November 1997 and was followed by a second prototype DA40-V2 (registered OE-VPE) which was powered by a Continental IO-240. In 1998 a third prototype DA40-V3 flew powered by a Lycoming IO-360 engine. Four more test aircraft were produced followed by the first production aircraft in 2000. JAR23 certification of the IO-360 production variant was obtained in October 2000. In 2002 the production of the Lycoming-engined variant was ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Aquila A 210
__NOTOC__ The Aquila A 210 is a two-seat reinforced plastic light aircraft produced in Germany from 2002. It remains in production in 2022 as the updated A211. Design and development The marketing name A 210 is usually used to refer to Aquila's light side by side two seat aircraft, though its official engineering and certification name is Aquila AT01. Design work started in 1997 and the first flight was made in March 2000. The A 210 is entirely built from carbon and glass fibre reinforced plastics (CFRP and GFRP). CRFP is used for the more highly stressed members, spars, frames and stringers, GFRP for shells and control surfaces, the latter with GFRP/polyurethane sandwich construction. The low wing has straight tapered inboard sections with increasing sweep outboard and winglets at the tips on production examples. It has a laminar flow section and 4.5° of dihedral. The ailerons are balanced and the inboard single slotted Fowler flaps have two positions. The A 210 is power ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
MSW Votec 221
The MSW Votec 221 is a single engine, single seat kitbuilt light-sport aircraft, designed and built in Switzerland. Design and development The Votec 221 is a single seat, low wing monoplane, designed for engines in the power range 90-180 kW (120-240 hp). The first prototype, completed in 2009, has a 157 kW (210 hp) Lycoming AEIO-390 flat-four engine and the second, finished the following year, a 134 kW (180 hp) engine. MSW's numerical designation has two digits indicating power in hp/10, followed by the number of seats, suggesting an optimum 220 hp power unit. Externally, the Votec 221 resembles a scaled down (span, 80%) MSW Votec 351. It has low aspect ratio straight tapered wings with blunt, almost square tips. Ailerons are assisted by external spades. The empennage is also straight tapered, with a forward set tailplane mounted on top of the fuselage, far enough forward on the fin to require only a small cut-out for movement of the deep ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Extra EA-300
The Extra Flugzeugbau EA300 is a two-seat aerobatic monoplane capable of Unlimited category competition. It was designed in 1987 by Walter Extra, a German aerobatic pilot, and built by Extra Flugzeugbau. Design and development Design of the Extra 300 was based on the Extra 230, an early 1980s monoplane having a wing made of wood. The Extra 300 has a welded steel tube fuselage covered in aluminium and fabric. The midset wing has a carbon fiber composite spar and carbon composite skins.Lambert 1993, p. 100. A symmetrical airfoil, mounted with a zero angle of incidence, provides equal performance in both upright and inverted flight. The landing gear is fixed taildragger style with composite main legs and fiberglass wheel pants. The powerplant is a fuel-injected Lycoming AEIO-540 which produces 300 horsepower (224 kW). The first two-seat Extra 300 made its maiden flight on 6 May 1988, with German type certification following on 16 May 1990. The single-seat Extra 300S flew ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
MSW Votec 252T
The MSW Votec 252T is a single engine kitbuilt light-sport aircraft with side-by-side seating for two, designed and built in Switzerland and was first flown in 2009. By October 2011 only this first prototype has flown. Design and development The Votec 252T is a side-by side seat development of MSW's earlier tandem seat Votec 322. The prototype, powered by a modified Lycoming IO-540-J3A5 flat-six engine, marries the wooden wings and empennage of the latter to a new, carbon fibre fuselage, though a carbon fibre wing is under development. All flying surfaces are straight tapered and square tipped, the wing low mounted and the tailplane located on the upper fuselage; the rudder extends down to the keel. The ailerons are balanced with external spades. The Votec 252T has a cabin over the wing, with baggage space behind the seat, under a single piece canopy. It has a fixed tricycle undercarriage with fuselage mounted cantilever legs and with speed fairings on all wheels. The nose ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Papa 51 Thunder Mustang
The Thunder Mustang is a modern 0.75 scale replica of the P-51 Mustang. It has joined the ranks of the high-performance P-51 kits alongside the Titan Aircraft T-51, which has a welded steel airframe with a secondary monocoque aluminum shell, the all-aluminum Stewart S-51D, and the full-scale, turbine-powered Cameron P-51G. Design and development The Thunder Mustang is currently in renewed production stages. Production ceased in the fall of 1999. The Thunder Builders Group LLC owned the assets required to manufacture the airplane in September 2010, when they sold the assets to Dean Holt of Mount Vernon, Washington. Dean is currently in the process of manufacturing all the necessary components for complete kit offerings, which will be available in late fall 2011. Operational history There were a total of 37 complete or partial kits produced, including the prototype. Of these 37, 27 were delivered as complete kits including the Falconer engine. Two have Walter turbines installed ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Grob Strato 2C
The Grob Strato 2C was a German experimental high altitude research aircraft. Powered by two turbocharged piston engines and featuring an extremely long span wing of composite construction, one aircraft was built in the 1990s, but was abandoned despite setting a world altitude record for piston-engined aircraft on its last flight. Development and design In April 1992, the German Aerospace Center (''Deutsches Zentrum für Luft- und Raumfahrt e.V'' - DLR) commenced a programme to develop an aircraft to carry out atmospheric, stratospheric and climatic research.Taylor, 1996, p.173. It chose Grob Aerospace to design and build an aircraft to meet these requirements, based both on its experience in use of composite material in aircraft structures together with its successful development of the Egrett surveillance aircraft, with the aircraft expected to be operational by 1996.Jeziorski ''Flight International'' 31 January - 6 February 1996, p.66. In order to meet the requirement to ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Pitts Model 12
The Pitts Model 12 (also known by its nicknames "Bolshoi", "Macho Stinker", "Pitts Monster") is a high performance aerobatic biplane designed around the Vedeneyev M14P/PF engine. The aircraft can be built from plans or as a kitplane, or can be bought ready-to-fly from the factory. Design and development The Pitts model 12 was designed by Curtis Pitts starting in 1993. Pitts presented his completed design on his 80th birthday in December 1995. The Pitts Model 12 is a biplane built using fabric covered welded steel tubing for the fuselage, and fabric covered wings with wood spars. The leading edge is made of formed plywood. The landing gear is solid aluminum Aluminium (aluminum in American and Canadian English) is a chemical element with the symbol Al and atomic number 13. Aluminium has a density lower than those of other common metals, at approximately one third that of steel. It ha .... Operational history , 59 examples had been completed and flown. V ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Fly-Fan Shark
The Fly-Fan Shark is a Slovak light aircraft designed by Frantisek Sustek and initially developed by Fly-Fan of Trenčín. Development continues under the new owner of the design, AENEA Services. The design was introduced at the AERO Friedrichshafen show in 2007 as a mock up and in 2011 as a flying aircraft. The aircraft first flew on 29 June 2011 and is intended to be supplied as a complete ready-to-fly-aircraft.Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 164. WDLA UK, Lancaster UK, 2011. ISSN 1368-485XTacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015-16'', page 150. Flying Pages Europe SARL, 2015. Design and development The Shark was designed with the goal of providing similar performance to other twin-engined light aircraft, but on 30% less power. It features a cantilever low-wing, a five-seat enclosed cabin, retractable tricycle landing gear and twin wing-mounted engines in tractor configuration ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Beriev Be-103
The Beriev Be-103 (in English sometimes called "Snipe") is an amphibious seaplane designed by Beriev and constructed by the Komsomolsk-on-Amur Aircraft Production Association (KnAAPO) in Russia. Intended for autonomous operation in the unmarked areas of Russia's far north and Siberia, the Be-103 was designed for short-haul routes in regions that have rivers, lakes and streams, but are otherwise inaccessible. Design and development The Be-103 is a mid-wing monoplane, making use of the modified wing roots as water-displacing sponsons. It features an all-moving slab tail and retractable tricycle landing gear for land operations. Its hallmark and most distinguishing design feature is the water-displacing wing, an unusual feature for a seaplane, with three aquaplaning implements (planing step, port and starboard wing trailing edges) which substantially enhance the aircraft's on-the-water stability and seaworthiness. The Be-103 features include an advanced, blended wing, swept at 22 ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
MSW Votec 352T
The MSW Votec 252T is a single engine kitbuilt light-sport aircraft with side-by-side seating for two, designed and built in Switzerland and was first flown in 2009. By October 2011 only this first prototype has flown. Design and development The Votec 252T is a side-by side seat development of MSW's earlier tandem seat Votec 322. The prototype, powered by a modified Lycoming IO-540-J3A5 flat-six engine, marries the wooden wings and empennage of the latter to a new, carbon fibre fuselage, though a carbon fibre wing is under development. All flying surfaces are straight tapered and square tipped, the wing low mounted and the tailplane located on the upper fuselage; the rudder extends down to the keel. The ailerons are balanced with external spades. The Votec 252T has a cabin over the wing, with baggage space behind the seat, under a single piece canopy. It has a fixed tricycle undercarriage with fuselage mounted cantilever legs and with speed fairings on all wheels. The nosew ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
