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  2. Limbach L275E - Wikipedia

    en.wikipedia.org/wiki/Limbach_L275E

    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.

  3. Limbach L550E - Wikipedia

    en.wikipedia.org/wiki/Limbach_L550E

    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 ...

  4. Limbach Flugmotoren - Wikipedia

    en.wikipedia.org/wiki/Limbach_Flugmotoren

    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 ...

  5. NASC TigerShark XP - Wikipedia

    en.wikipedia.org/wiki/NASC_TigerShark_XP

    Engine 32 Hp Herbrandson 372cc two stroke. Autopilot Fully Autonomous Piccolo II [2] References This page was last edited on 4 November 2024, at 01:25 (UTC). ...

  6. Rotax 447 - Wikipedia

    en.wikipedia.org/wiki/Rotax_447

    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 ...

  7. TechProAviation Merlin 100 - Wikipedia

    en.wikipedia.org/wiki/TechProAviation_Merlin_100

    The standard engine used is the 35 hp (26 kW) Verner JCV 360 twin cylinder four-stroke powerplant. Alternative engines include the 60 hp (45 kW) HKS 700E four-stroke, 50 hp (37 kW) Hirth F-23 and 64 hp (48 kW) Rotax 582 two-stroke powerplants. The aircraft will be marketed as a kit only. [1] [2] [3]

  8. Ivchenko-Progress AI-322 - Wikipedia

    en.wikipedia.org/wiki/Ivchenko-Progress_AI-322

    The development of the engine continues at Ivchenko-Progress of Zaporizhzhia, Ukraine. The engine was originally intended for the Hongdu L-15 trainer aircraft and it is now planned to be used in Baykar Bayraktar Kızılelma fighter UAV. An afterburning version, the AI-322F is also available.

  9. ATE Vulture - Wikipedia

    en.wikipedia.org/wiki/ATE_Vulture

    The ATE Vulture is a South African unmanned aerial vehicle (UAV) designed and built by Advanced Technologies and Engineering (now Paramount Advanced Technologies, a division of the Paramount Group). It is powered by a 500 cc 2-stroke fuel injected engine. Its payload is a gyro stabilised optronic sight communicating on a secure C-Band data ...

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