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词条 IAR 95
释义

  1. Design and development

  2. Specifications

  3. See also

  4. References

  5. External links

name= IAR 95image= IAR 95 Spey (model).jpgcaption=Model of the final design
}}{{Infobox Aircraft Type
type = Fighter/ground attack aircraftnational origin = Romaniamanufacturer = Avioane Craiovadesigner = INCAS Romaniafirst flight =introduction =retired =status = Project cancelled in 1988primary user = Romanian Air Forcemore users =produced =number built = Noneprogram cost =unit cost =developed from =variants with their own articles =developed into =
}}

The IAR 95 Spey was a Romanian project to produce a supersonic fighter jet for the Romanian Air Force. The project was started in the late 1970s and cancelled in 1981. Shortly after, the project was restarted again. The project was cancelled for good in 1988 due to lack of funds before a prototype could be built, although a full-scale mockup was being constructed.[1]

Design and development

The design was a high-wing monoplane with lateral air intakes, a single fin, and a single engine. Designs with two fins and two engines were also considered, but it was decided to go with the single-engine single-fin design. Other designations given to this project are IAR-101 and IAR-S and refer to different design layouts.

Romania considered a joint program with Yugoslavia, but the latter declined because it was designing its own supersonic fighter jet, the Novi Avion.

Specifications

The following technical data applies to the design that progressed the furthest:

{{aircraft specifications
|plane or copter?=plane
|jet or prop?=jet
|ref= IAR 95 specifications[1]
|crew=One or two
|length main=16 m
|length alt=52 ft 6 in
|span main=9.3 m
|span alt=30 ft 6 in
|height main=5.45 m
|height alt=17 ft 11 in
|area main= 27.9 m²
|area alt=300.3 ft²
|empty weight main=7,880 kg
|empty weight alt=17,372 lb
|max takeoff weight main=15,200 kg
|max takeoff weight alt=33,510 lb
|engine (jet)=Tumansky R-29-300
|type of jet=with afterburner
|number of jets=1
|thrust main=81.4 kN
|thrust alt=18,300 lbf
|afterburning thrust main=122kN
|afterburning thrust alt=27,500 lbf
|armament=
  • 3200 kg (7,055 lb) of various missiles and bombs

}}

See also

  • FMA SAIA 90
{{aircontent
|see also=
|similar aircraft=
  • Dassault Mirage F-1
  • JF-17 Thunder
  • Novi Avion

|lists=
  • List of fighter aircraft

}}

References

1. ^Romanian Supersonic Project
  • Romanian National Institute for Aerospace Research INCAS S.A.
  • International Air Power Review, Winter 2001-2002

External links

{{commons category|IAR aircraft}}
  • National Institute for Aerospace Research "Elie Carafoli" - Romanian Supersonic Projects, IAR-95

Romanian Supersonic Projects

{{IAR Aircraft}}

3 : Cancelled military aircraft projects|IAR aircraft|Romanian fighter aircraft 1980–1989

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