Mustang Aeronautics Mustang II. Specifications. A photo.
Mustang Aeronautics Mustang II - light multipurpose aircraft designed «Mustang Aeronautics» specialists of the American aircraft manufacturer / and manufactured with 1966 years.
Mustang Aeronautics Mustang IIa photo
Start of work on the construction Mustang Aeronautics Mustang II multipurpose aircraft was initiated in 1964 year, at the same time as the base of the base American experts took the previous model Mustang Aeronautics Midget Mustang, further optimize the design of the aircraft, which in turn allowed to carry on board already two people.
The aircraft model Mustang Aeronautics Mustang II has high maneuverability and can be used as a sports aircraft for which the aircraft in nature and has been developed. However, subsequently, to the aircraft showed a hefty interest and private customers, and therefore the production of aircraft Mustang Aeronautics Mustang II and continues to this day. In addition, due to the paired control, the aircraft can be used for training future pilots piloting skills, the more that predisposes to this relatively low cost, made according to the order, the middle 2015 45 thousand dollars, depending on the configuration of the aircraft.
A photoMustang Aeronautics Mustang II
aircraft cabin has a sufficiently small size, and therefore allows you to stay on board just two people, and, transportation in an airplane any goods are not available, due to which the popularity of the aircraft is not so big - with 1966 on 2011 year was built 480 this model aircraft.
Due to the good aerodynamic shape, the plane can be accelerated to a maximum velocity in 370 km \ h., With the fuselage of the aircraft has been greatly enhanced by developers at the design stage, which in turn provides the aircraft opportunity to resist even highly significant positive or negative overloads.
AircraftMustang Aeronautics Mustang II
The basic version of Mustang Aeronautics Mustang II model involves the use of a piston power plant consisting of a four-cylinder aircraft engine Lycoming O-320 160 power in HP If necessary, there may be used, and a more powerful and productive power plant - four-cylinder aircraft engine Lycoming IO-360 able to develop traction in 200 hp and disperse the aircraft up to speed in 405 km \ h. However, the maximum flight range of the aircraft is very limited and is only 692 kilometers, which does not allow a broad sense to use all capabilities of the aircraft.
Specifications Mustang Aeronautics Mustang II.
- Crew: 1 chelvoeka;
- Passenger: 1 people;
- aircraft Length: 5,94 m .;
- Wingspan: 7,38 m .;
- Plane Height: 1,6 m .;
- Weight of empty aircraft: 420 kg. (Depending on version);
- Payload: 260 kg. (Depending on version);
- Maximum takeoff weight: 680 kg. (Depending on version);
- Cruising speed: 320 km \ h. (Depending on version);
- Maximum flight speed: 370 km \ h. (Depending on version);
- Maximum flight distance: 692 km .;
- Maximum flight height: 6400 m .;
- aircraft engine type: a piston;
- Powerplant: Lycoming O-320 (depending on version);
- Power: 160 hp (Depending on version).
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