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The first Cub Cadet model made was the International Cub Cadet Tractor, better known as the Original. The Cub Cadet Original was powered by a 7 hp and 8 hp replacement Kohler engine and was made between 1961 and 1963. The CJR was a hydrostatic version of the Cub Cadet transmission made by Sundstrand Corporation.
The Rotax 582 is based upon the earlier Rotax 532 engine design and was designed for ultralight aircraft. [ 4 ] [ 5 ] The 582 increased the bore from the 532 engine's 72 to 76 mm (2.8 to 3.0 in). This increased the displacement from 521.2 cc (31.81 cu in) to 580.7 cc (35.44 cu in), an increase of 11%.
The standard engine includes a muffler exhaust system and an intake air filter. The standard starter is a recoil start type, with an electric starter optional. An integral alternating current generator produces 12 volts. [1] The Rotax 532 was replaced in production by the improved Rotax 582 engine design. The 582 increased the cylinder bore ...
The engines were developed as competitors to the 64 hp (48 kW) Rotax 582 with an identical mounting bolt pattern to the 582, allowing either to be a drop-in replacement. The engines are similar to the Rotax powerplant in being liquid-cooled, two-cylinder in-line engines, with dual capacitor discharge ignition. The 3502 was developed from the ...
In 1981 the Cub Cadet product line was acquired from International Harvester, and the White Outdoor Products Company was acquired from the old White Motor Company. In 1985 the company's Martin, Tennessee plant began operation, and Arnold Corporation was acquired. In 1986 Aircap Industries in Tupelo, Mississippi was acquired.
Data from Lockwood Aircraft & Kitplanes General characteristics Crew: one Capacity: one passenger and 505 lbs (229 kg) useful load Length: 22 ft 0 in (6.71 m) Wingspan: 30 ft 0 in (9.15 m) Height: 10 ft 0 in (3.05 m) Wing area: 160 sq ft (14.88 m 2) Empty weight: 495 lb (224 kg) Max takeoff weight: 1,000 lb (454 kg) Powerplant: 1 × Rotax 912 UL four stroke piston engine, 80 hp (60 kW ...
The MZ 202 was developed first as a 60 hp (45 kW) lightweight competitor to the liquid-cooled 64 hp (48 kW) Rotax 582.Later the MZ 201 was developed from the MZ 202 as a de-rated 45 hp (34 kW) version intended for motorgliders and single place ultralights that needed more power than the single-cylinder Zanzottera MZ 34.
Two seats in side-by-side configuration, high wing ultralight, powered by an 80 hp (60 kW) Rotax 912UL engine, the 100 hp (75 kW) Rotax 912ULS or the 85 hp (63 kW) Jabiru 2200. The Xtra underwent an aerodynamic cleanup by aerodynamicist Barnaby Wainfan and was introduced in 1999. Variously marketed as the Mark III Xtra and the M3X. [5] [7]
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