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The Rotax 503 is a 37 kW (50 hp), inline 2-cylinder, two-stroke aircraft engine, built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft. [ 1 ] [ 2 ] For decades the engine was one of the most popular and reputedly reliable aircraft engines in its class (two-stroke, under 60 horsepower), [ 3 ] and it remains widely used and ...
The standard engine supplied was the twin cylinder, liquid-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine in pusher configuration. The 50 hp (37 kW) Rotax 503 and 40 hp (30 kW) Rotax 447 engines were factory options. [1] The aircraft fuselage is made from metal tubing, while the fairing is fiberglass. Its two-bladed rotor has ...
Data from Kitplanes and Aerocrafter General characteristics Crew: One Length: 17 ft 0 in (5.18 m) Wingspan: 29 ft 6 in (8.99 m) Wing area: 127 sq ft (11.8 m 2) Empty weight: 325 lb (147 kg) Gross weight: 587 lb (266 kg) Fuel capacity: 9 US gallons (34 litres) Powerplant: 1 × Rotax 503, 50 hp (37 kW) Propellers: 2-bladed wooden Performance Maximum speed: 95 mph (153 km/h, 83 kn) Cruise speed ...
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 ...
Data from Taylor 1996 General characteristics Crew: One Capacity: One passenger Length: 20 ft 0 in (6.10 m) Wingspan: 34 ft 6 in (10.52 m) Empty weight: 440 lb (200 kg) Gross weight: 930 lb (422 kg) Powerplant: 1 × Rotax 582, 64 hp (48 kW) Propellers: 2-bladed wooden Performance Maximum speed: 120 mph (190 km/h, 100 kn) Cruise speed: 90 mph (140 km/h, 78 kn) Range: 220 mi (350 km, 190 nmi ...
The aircraft has a standard empty weight of 235 lb (107 kg). It features a Hi-Pro 370 sq ft (34 m 2) parachute-style wing, single-place accommodation, tricycle landing gear and a single 50 hp (37 kW) Rotax 503 engine. [1] The aircraft carriage is built from aluminium tubing. In flight steering is accomplished via foot pedals that actuate the ...
To enable the Taurus to self-launch, a pop-out propeller is mounted on the rear fuselage driven by a Rotax 503 piston engine. [2] In 2007 the company developed the Taurus Electro with the piston engine replaced by a permanent magnet synchronous three-phase brushless motor. [3] [9] By 2011, Pipistrel had delivered 100 aircraft of the Taurus ...
Data from Cliche and SlipStream General characteristics Crew: one Capacity: one passenger Length: 19 ft 4 in (5.89 m) Wingspan: 30 ft 8 in (9.35 m) Height: 6 ft 3.5 in (1.918 m) Wing area: 154 sq ft (14.3 m 2) Empty weight: 465 lb (211 kg) Gross weight: 1,100 lb (499 kg) Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 503 twin cylinder, two-stroke aircraft engine, 50 hp (37 kW ...