Novi Avion

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Novi Avion
Novi avion YU.JPG
Type: Multipurpose fighter
Design country:

Yugoslavia Socialist Federal RepublicYugoslavia Yugoslavia

Manufacturer:

Yugoslav Aeronautical Engineering Institute , Soko

First flight:

planned for 1992, according to other sources for 1995

Commissioning:

Mid-1990s (planned)

Number of pieces:

150 (planned)

The Novi Avion (in German: New Airplane ) was a planned Yugoslav single - engine multi- role fighter aircraft .

history

In the mid-1980s, the Yugoslav Aeronautical Institute began work on a fighter aircraft that would replace the older MiG-21 in the Yugoslav Air Force. The project was carried out under the name Novi Avion . An alternative name, perhaps later the official name, was supersonic . Up to 150 units were planned. The first flight of a prototype was planned for 1992. As an interim solution up to the introduction of the Novi Avion, the Yugoslav Air Force ordered 50 MiG-29s , of which 14 MiG-29B and 2 MiG-29UB were delivered until the breakup of Yugoslavia. With the disintegration of Yugoslavia in 1991, the project was canceled and finally discontinued.

The French Rafale , which was also in the development stage, served as a model for the Novi Avion . Accordingly, Dassault Aviation was also involved in the project, some parts of the aircraft would have been produced in France. The Novi Avion would basically have been a simplified and cheaper version of the Rafale, with only one engine instead of two as in the French model. The Snecma M88 was intended as the engine . The on-board radar Cyrano IVMR as in the Mirage F1 or RDM / RDI as in the Mirage 2000 might have been used. Dassault estimated a possible export opportunity for the aircraft at 300 to 500 units.

Technical specifications

Parameter Computational data
crew 1
length 13.75 m
span 8.00 m
height 4.87 m
Wing area 30.00 m²
Wing loading maximum (max. takeoff weight): 446.67 kg / m²
Empty mass 6,247 kg
Max. Takeoff mass 13,400 kg
Load factor up to +8.84 g
Top speed 2,000 km / h or Mach 1.88
Service ceiling 17,000 m
Range 3,765 km
Max. Gun load 4,500 kg at 11 external load stations (9 of them under the wings
and under the fuselage and two on the wing tips)
Engine a Snecma M88 turbofan engine

Armament

Individual evidence

  1. Airserbia - project insight with the general staff of the JNA
  2. Short article on the role of Dassault on Flightglobal (archive)
  3. harpoondatabases.com ( Memento from December 1, 2008 in the Internet Archive )