Search results
Results from the WOW.Com Content Network
The Ivchenko-Progress AI-450S is a turboprop engine designed by Ivchenko-Progress and built by Motor Sich. [citation needed] It is a two-shaft design with one gas generator shaft and one free turbine shaft. The 450 hp AI-450S is used on the Diamond DA50-JP7, Bayraktar Akıncı UAV and Diamond Dart 450 and the 630 hp AI-450S-2 is used on the ...
Data from OPERATORS MANUAL FOR ENGINE TYPES 447, 503 & 582 General characteristics Type: two-stroke air-cooled aeroengine Bore: 67.5 mm (2.66 in) Stroke: 61 mm (2.4 in) Displacement: 426.5 cc (26.64 cu in) Dry weight: 26.8 kg (59 lb) (dry, no exhaust system) Components Valvetrain: piston ports Fuel system: pneumatic pump pressurized Fuel type: regular autofuel Oil system: premixed in the fuel ...
Rotax is one of the world's principal suppliers of aircraft engines for ultralight aircraft, light aircraft and unmanned aerial vehicles. [2] Between 1985 and 1995, 60,000 Rotax engines were sold for aircraft propulsion. [2] In the light aircraft class, in 1998 Rotax outsold all other aero engine manufacturers combined. [4]
The Rotax 912 was first sold in 1989 in non-certificated form for use in ultralights and motorgliders. [3]The original 80 hp (60 kW) 912 UL engine has a capacity of 1,211 cc (73.9 cu in) and a compression ratio of 9.1:1, and is designed to work with regular automotive gasoline, with up to 10% ethanol.
Ukrspecsystems PD-2 is a Ukrainian multi-purpose unmanned aerial vehicle (UAV). It is designed for aerial reconnaissance and for combat use as a carrier of bombs with warheads weighing up to 3 kg (6.6 lb). [1] The aircraft can take off from a runway, or be equipped with removable modules for vertical take-off and landing.
However, with a manual transmission engine RPM can redline in "neutral", or by shifting to a higher gear too late, or by shifting to a lower gear too early. In the case of "neutral" or shifting up too late, a rev limiter can easily keep engine RPM below the redline. If a manual transmission is shifted down too early, the speed of the vehicle ...
Culver LFA Cadet at Museo Nacional Aeronáutico y del Espacio, Chile Cadet LCA Initial production version powered by a 75 hp (56 kW) Continental A75-8. Cadet LFA Improved variant with an 80 hp (60 kW) Franklin 4AC-176-F3, Franklin 4AC-176-D2, or Franklin 4AC-176-D3 engine, and a full electrical system and engine starter.
The Wing Loong II UAV MALE is an enlarged version of the Wing Loong I with a longer body and wider wing span. It has a slender fuselage, V-tail , and ventral fin. The aircraft features retractable landing gear, including two main wheels under the fuselage and one single wheel under the nose.