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Mustang Aeronautics Mustang II. Specifications. A photo.
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Mustang Aeronautics Mustang II. Specifications. A photo.

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 Mustang Aeronautics Mustang II has a high maneuverability and can be operated as a sport aircraft, for which the aircraft was inherently designed. Nevertheless, later, private aircraft showed considerable interest in the aircraft, and the production of the Mustang Aeronautics Mustang II aircraft continues to this day. In addition, thanks to the twin control, the aircraft can also be used for training the skills of piloting future pilots, especially since it is predisposed by a rather low cost, which according to the mid-2015 data is about 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 the model Mustang Aeronautics Mustang II provides for the use of a piston power plant consisting of one four-cylinder aircraft engine Lycoming O-320 with an output of 160 hp. If necessary, a more powerful and efficient propulsion system can be used here-the Lycoming IO-360 four-cylinder aircraft engine capable of developing thrust in 200 hp, and accelerating the aircraft to a speed of 405 km / h. Nevertheless, the maximum range of the flight of this aircraft is very limited and is only 692 kilometers, which does not allow in a broad sense to use all the 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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