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  2. Rotax 916 iS - Wikipedia

    en.wikipedia.org/wiki/Rotax_916_iS

    Cub Crafters said of the engine that the "key to the development of the new aircraft is CubCrafters’ collaboration with BRP-Rotax, which is launching their new 160 HP turbocharged engine on the Carbon Cub UL. The new 916 iS engine is lighter, more fuel efficient, and can produce more power than the normally aspirated CC340 engine on the ...

  3. Rotax 914 - Wikipedia

    en.wikipedia.org/wiki/Rotax_914

    The Rotax 914 is a turbo-charged, four-stroke, four-cylinder, horizontally opposed aircraft engine with air-cooled cylinders and water-cooled cylinder heads.It is designed and built by the Austrian company BRP-Powertrain, owned by Bombardier Recreational Products (BRP), as part of its Rotax brand.

  4. Rotax 915 iS - Wikipedia

    en.wikipedia.org/wiki/Rotax_915_iS

    The Rotax 915 iS is a four-cylinder four-stroke, horizontally-opposed, turbocharged, air and liquid-cooled, gasoline engine design, with a mechanical gearbox reduction drive. The turbocharger has a compression ratio of 3.5:1 and the engine will have a critical altitude of 15,000 ft (4,572 m).

  5. Rotax 912 - Wikipedia

    en.wikipedia.org/wiki/Rotax_912

    The Rotax 912 was first sold in 1989 in non-certificated form for use in ultralights and motorgliders. [3]The original 60 kW (80 hp) 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.

  6. Rolls-Royce RR500 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_RR500

    The Rolls-Royce RR500 is a family of small gas turbine engines developed by Rolls-Royce Corporation.The RR500TP turboprop variant was intended for use in small aircraft. The RR500TS was the turboshaft variant designed for light helicopters.

  7. QAC Quickie Q2 - Wikipedia

    en.wikipedia.org/wiki/QAC_Quickie_Q2

    Data from QuickieBuilders and Western Canada Aviation Museum General characteristics Crew: one pilot Capacity: one passenger and 510 lb (231 kg) useful load Length: 19 ft 10 in (6.05 m) Wingspan: 16 ft 8 in (5.08 m) Height: 4 ft 5 in (1.35 m) Wing area: 67 sq ft (6.22 m 2) Empty weight: 490 lb (222 kg) Max takeoff weight: 1,000 lb (454 kg) Powerplant: 1 × Revmaster 2100-DQ converted auto ...

  8. CFM Shadow - Wikipedia

    en.wikipedia.org/wiki/CFM_Shadow

    Data from Pilot manuals and owner knowledge General characteristics Crew: 2 Length: 6.405 m (21 ft 0 in) Wingspan: 10.015 m (32 ft 11 in) Height: 2.490 m (8 ft 2 in) Wing area: 15.26 m 2 (164 sq ft) Empty weight: 196 kg (432 lb) Maximum ZFW Gross weight: 386 kg (851 lb) Max takeoff weight: 386 kg (851 lb) Fuel capacity: 24L Main + 30L Slipper = 54L Powerplant: 1 × Rotax 582UL two-cylinder ...

  9. William Frost - Wikipedia

    en.wikipedia.org/wiki/William_Frost

    William Frost was born on 28 May 1848 in Saundersfoot, Pembrokeshire, to Rebecca and John Frost.. His ambition to invent a flying machine started about 1880. [1] Despite his poverty he constructed the "Frost Airship Glider", which seems, in principle, to have resembled a vertical takeoff airplane, with gas-filled tanks.