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IAR 95

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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
229:. 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. 467:
Security Assistance, U.S. And International Historical Perspectives: Proceedings of the Combat Studies Institute 2006 Military History Symposium
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engine, 81.4 kN (18,300 lbf) thrust dry, 122 kN (27,000 lbf) with afterburner
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The following technical data applies to the design that progressed the furthest:
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3,200 kg (7,055 lb) of various missiles and bombs
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Aircraft of comparable role, configuration, and era
46:. Unsourced material may be challenged and removed. 1003: 534: 345:1,500 km/h (930 mph, 810 kn) 541: 527: 497:International Air Power Review. Compendium 232: 218:Spey was a Romanian project to produce a 106:Learn how and when to remove this message 241:Romania considered a joint program with 1004: 494: 118:Romanian cancelled jet fighter project 522: 1012:Cancelled military aircraft projects 499:(1st ed.). Airtime Publishing. 44:adding citations to reliable sources 15: 295:5.45 m (17 ft 11 in) 13: 550:Industria Aeronautică Română (IAR) 488: 14: 1033: 514: 301:27.9 m (300 sq ft) 289:9.3 m (30 ft 6 in) 252: 495:Donald, David, ed. (June 2001). 396: 382: 283:16 m (52 ft 6 in) 129: 20: 1022:1980s Romanian fighter aircraft 313:15,200 kg (33,510 lb) 31:needs additional citations for 470:. 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"IAR 95"
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Romania
Manufacturer
Avioane Craiova
Romanian Air Force
supersonic
fighter
Romanian Air Force
Yugoslavia
Novi Avion
Tumansky R-29
afterburning
turbojet
Romania portal
Aviation portal
FMA SAIA 90
Dassault Mirage F-1
JF-17 Thunder
Novi Avion

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