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The L550E is an air-cooled horizontally-opposed 550cc four-cylinder two-stroke petrol engine developing 37 kW (50 hp) at 7500 rpm which can drive a propeller either directly or geared. It employs a single magneto ignition, four carburettors , and is lubricated by oil mixture lubrication with a fuel to oil ratio of 25:1 for mineral oil or 50:1 ...
The L275E is a twin cylinder horizontally-opposed two-stroke, air-cooled, direct-drive petrol engine design, based upon the Volkswagen air-cooled engine.It employs a single magneto ignition, two carburettors, is lubricated by oil mixture lubrication with a fuel to oil ratio of 25:1 for mineral oil or 50:1 for synthetic oil and produces 15 kW (20 hp) at 7200 rpm.
The larger engines, some 2000cc and all 2400cc, are based on the Volkswagen Wasserboxer engine. The most powerful versions of the 2400cc engines have water cooled cylinder heads as well as electronic fuel injection and electronic ignition. Limbach also makes two-stroke engines for UAV as well as uncertified versions of a few four-stroke engines ...
Unmanned aerial vehicles (UAVs) Aircraft engines; 0–9. 2si ... Ceskoslovenska Zbrojovka ZOD 260-B 2-stroke radial diesel engine – 260 hp [19] CFM International
The AAI RQ-2 Pioneer is an unmanned aerial vehicle (UAV) that was used by the United States Navy, Marine Corps, and Army, and deployed at sea and on land from 1986 until 2007. Initially tested aboard USS Iowa , the RQ-2 Pioneer was placed aboard Iowa -class battleships to provide gunnery spotting, its mission evolving into reconnaissance and ...
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 ...
Data from Unmanned Aircraft Directory General characteristics Crew: None Capacity: 50 kg (110 lb) payload Length: 4.00 m (13 ft 1 in) Wingspan: 4.73 m (15 ft 6 in) Height: 1.27 m (4 ft 2 in) Wing area: 3.0 m 2 (32 sq ft) Max takeoff weight: 408 kg (899 lb) Powerplant: 1 × Herbrandson Dyad 2-cylinder, 2-stroke piston engine, 19 kW (26 hp) Performance Maximum speed: 180 km/h (110 mph, 97 kn ...
The TigerShark XP is an unmanned aerial vehicle developed by Navmar Applied Sciences Corporation. [1] Specifications ... Engine 32 Hp Herbrandson 372cc two stroke.
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