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The aircraft was designed to comply with the US Experimental – Amateur-built and European microlight aircraft rules. It features a single main rotor and tail rotor, a single-seat enclosed cockpit with a windshield, skid landing gear and a two-cylinder, air-cooled, two stroke 64 hp (48 kW) MZ 202 engine.
The Solar T62 Titan is an American gas turbine engine used mainly as a aircraft auxiliary power unit (APU), conventional power generator, turboprop engine for fixed-wing aircraft or turboshaft engine for helicopters. A new turbine version was developed as the Solar T66.
The Mosquito Air was designed to comply with the United States FAR 103 Ultralight Vehicles, including the category's maximum empty weight of 254 lb (115 kg). The aircraft has a standard empty weight of 254 lb (115 kg).
LHTEC (Light Helicopter Turbine Engine Company) is a joint venture between Rolls-Royce and Honeywell. The company was originally a partnership between the Allison Engine Company and AlliedSignal Aerospace. [1] In 1995 Rolls-Royce acquired Allison, and AlliedSignal merged with Honeywell in 1999, and adopted its name.
Voytovich helicopter Ukraine [31] Kazachok Helicopter Russia [32] Kazan Aktai: Russia Rotorfly Russia [33] Berkut (helicopter) Russia FLY CC III Czech Republic [34] jpkrucker Canada Single seat coaxial heli [35] Mosquito XE: Canada / United States Hungarocopter HC-01: Hungary [36] Hungarocopter HC-02: Hungary [37] CoaX helicopters Australia [38 ...
It is produced by the LHTEC (Light Helicopter Turbine Engine Company), a joint venture between Rolls-Royce and Honeywell. The commercial and export version is the CTS800 . The engine was primarily developed for the United States Army 's cancelled RAH-66 Comanche armed reconnaissance helicopter, but has found use in other applications.
The General Electric T64 is a free-turbine turboshaft engine that was originally developed for use on helicopters, but which was later used on fixed-wing aircraft as well. General Electric introduced the engine in 1964. The original engine design included technical innovations such as corrosion resistant and high-temperature coatings. [1]
Turboshaft engine with a maximum and normal power rating of 2,200 and 1,850 shp (1,640 and 1,380 kW) and a pressure ratio of 6:1; high-speed version of the T55-L-3 [21] allowed for use on the Chinook instead of the geared YT55-L-3 engine due to August 1958 engine contract modification, with the reduction gearing now provided in the helicopter ...