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  2. Rotax - Wikipedia

    en.wikipedia.org/wiki/Rotax

    Rotax is the brand name for a range of internal combustion engines developed and manufactured by the Austrian company BRP-Rotax GmbH & Co KG [1] (until 2016 BRP-Powertrain GmbH & Co. KG), in turn owned by the Canadian Bombardier Recreational Products (BRP). Under the Rotax brand, the company is one of the world's largest producers of light ...

  3. Comparison of orbital rocket engines - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    This page is an incomplete list of orbital rocket engine data and specifications. Current, upcoming, and in-development rocket engines. Engine ... 1,630: 2.65: RD-809K

  4. Template:Aircraft specifications/doc - Wikipedia

    en.wikipedia.org/wiki/Template:Aircraft...

    This template has provisions for four sections: General characteristics, performance, armament, and avionics. What follows is list of the parameters that appear in each section, and specialised instructions for their use where necessary.

  5. Ikarus C42 - Wikipedia

    en.wikipedia.org/wiki/Ikarus_C42

    The Ikarus C42 is a single-engined high-wing monoplane with side-by-side seats for two in a 1.22 m (48 in) wide cabin. The C42 is manufactured with either an 80 hp (60 kW) Rotax 912 engine or a 100 hp (75 kW) Rotax 912s engine. The Rotax engine has a low fuel consumption and relatively low noise.

  6. BRM Aero Bristell - Wikipedia

    en.wikipedia.org/wiki/BRM_Aero_Bristell

    Data from AVweb and company website General characteristics Crew: one Capacity: one passenger Length: 6.45 m (21 ft 2 in) Wingspan: 8.13 m (26 ft 8 in) Height: 2.28 m (7 ft 6 in) Wing area: 10.5 m 2 (113 sq ft) Empty weight: 290 kg (639 lb) Gross weight: 472.5 kg (1,042 lb) Fuel capacity: 120 litres (26 imp gal; 32 US gal) Powerplant: 1 × Rotax 912ULS, 75 kW (100 hp) Performance Cruise speed ...

  7. Van's Aircraft RV-12 - Wikipedia

    en.wikipedia.org/wiki/Van's_Aircraft_RV-12

    The RV-12iS is an incremental improvement over the RV-12 which allows the installation of the Rotax 912ULS (carbureted) or the Rotax 912iS (fuel-injected) engines. It also incorporates a new cowling and throttle quadrant design, quick-retracting flaps, a quick-adjusting seat, redesigned landing gear attachments and fuel tank, among other ...

  8. Flight Design CT - Wikipedia

    en.wikipedia.org/wiki/Flight_Design_CT

    The standard engines for this version are 80 hp (60 kW) Rotax 912UL, the 100 hp (75 kW) Rotax 912ULS and the 115 hp (86 kW) Rotax 914 four-stroke powerplants. [4] [20] Remained in production in 2017. [14] F2 Model introduced in 2020, designed specifically for flight training as well as private owners.

  9. Template:Aircraft specs - Wikipedia

    en.wikipedia.org/wiki/Template:Aircraft_specs

    Template:Aircraft specs displays aircraft specifications, automatically formatted and converted for either metric or imperial units. Usage A "note" parameter is available for every parameters for qualifying the entry.