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Improved production model with a 40 hp (30 kW) Rotax 447 engine. [4] [6] [7] [8] [10] Weedhopper 40 Current production model with a 40 hp (30 kW) Rotax 447 engine. [3] [5] [9] [1] Weedhopper Super Up-engined model with a 50 hp (37 kW) Rotax 503 engine, many extras and an empty weight of 330 lb (150 kg) for the US amateur-built category. [9] [10 ...
The CB-40 was re-engineered to overcome problems of vibration and cooling in the original design. [2] Suited for ultralight use and single seat light sport aircraft, the engine weighs 86 lbs and produces 40 hp (30 kW). The engine uses a short aluminum crankcase with redesigned oil galleries for improved lubrication.
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 ...
Aventura UL Single seater optimised for the US FAR 103 Ultralight Vehicle category, with an empty weight of 328 lb (149 kg). Engines include the original 28 hp (21 kW) Rotax 277 in early models and the 40 hp (30 kW) Rotax 447 currently. 90 had been completed and flown by the end of 2011.
The Teledyne CAE J402 is an American small turbojet engine. Several variants have been developed to power unmanned air vehicles such as missiles and target drones. Developed in the 1970s for the Harpoon anti-ship missile, the J402 was the first jet engine to be designed as a "wooden round", meaning that the engine had to be able to sit for long periods without maintenance or inspection and ...
Data from Cuyuna & McCornack General characteristics Type: Direct drive two-stroke piston aircraft engine Bore: 2.658 in (68 mm) Stroke: 2.362 in (60 mm) Displacement: 428 cc (26.11 cubic inches) Dry weight: 65 lb (29 kg) Designer: McCornack/Cuyuna Components Fuel type: Regular auto fuel Oil system: 40:1 premixed fuel and oil Cooling system: fan forced air Performance Power output: 30 hp (22 ...
Data from Cliche & Tennessee Propellers General characteristics Type: Two cylinder, two-stroke aircraft engine Bore: 72 mm (2.8 in) Stroke: 59.5 mm (2.3 in) Displacement: 484 cc (29.54 cu in) Length: 14.96 in (380.0 mm) Width: 23.39 in (594.1 mm) Height: 15.00 in (381.0 mm) Dry weight: 90 lb (40.8 kg) equipped with reduction drive, electric start and muffler Components Valvetrain: piston ...
The design is a four-cylinder, two-stroke, piston diesel engine, in an inverted-V configuration, with turbocharging and supercharging, mechanical fuel injection, liquid cooling, direct drive. It can run on Jet-A or sustainable aviation fuel. The manufacturer claims that it has "40 percent fewer moving parts than other engines in its category ...
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