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The result was the Space Bug .049 Contest engine, Cox's first model plane engine which was completed in October 1951. [8] In 1952 the first name change was made to L.M. Cox Manufacturing Company Inc. The Space Bug engine set the scene for all the Cox engines that followed, and went into full production in 1952.
Pages in category "Two-stroke aircraft piston engines" The following 81 pages are in this category, out of 81 total. This list may not reflect recent changes.
Two-stroke model engines, most often designed since 1970 with Schnuerle porting for best performance, range in typical size from .12 cubic inches (2 cubic centimeters) to 1.2 ci (19.6 cc) and generate between .5 horsepower (370 watts) to 5 hp (3.7 kW), can get as small as .010 ci (.16 cc) and as large as 3-4 ci (49–66 cc). [2] Four-stroke ...
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 ...
The Rotax 532 is a 48 kW (64 hp) two-stroke, two-cylinder, rotary valve engine, liquid-cooled, gear reduction-drive engine that was formerly manufactured by BRP-Rotax GmbH & Co. KG. It was designed for use on ultralight aircraft. [1]
The 2si 460 is a family of in-line twin-cylinder, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft. [1]The basic engine was originally designed and produced by ILO-Motorenwerke of Germany and was later acquired by the AMW Cuyuna Engine Company of Beaufort, South Carolina and marketed under the Cuyuna brand name.
Global Motors originally designed a Half VW engine for use in light aircraft. The company and its designs were then sold to Mosler Motors. Warren Mosler specialized in racing engines and added the engine to the list of products eventually marketed under the company name Total Engine Concepts. The engine was dropped from production in 1998. [1]
It is equipped with a recoil starter system or optionally electric start and a 2.5 or 2.8:1 belt reduction drive. [1] [2] [3] The engine runs on a mixture of unleaded auto fuel and oil. [1] [2] Producing 22 hp (16 kW) at 6600 rpm, the G-25 competed in the early 1980s ultralight powerplant market against the similar Rotax 277. Production of the ...
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