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Avioane IAR 93 Vultur (Vulture)

Romania (1979)

Detailing the development and operational history of the Avioane IAR 93 Vultur (Vulture) Light Strike / Low Altitude Interceptor Aircraft.

 Entry last updated on 8/29/2017; Authored by Staff Writer; Content ©www.MilitaryFactory.com



  Avioane IAR 93 Vultur (Vulture)  
Picture of Avioane IAR 93 Vultur (Vulture) Light Strike / Low Altitude Interceptor Aircraft


The IAR 93 Vulture served with the Romanian Air Force for nearly two decades before seeing retirement in 1998.

Romania and Yugoslavia managed autonomy in the Soviet-dominated socialist period following World War 2. As such, the countries paired in 1971 to produce a light ground attack combat aircraft with interceptor capabilities for their respective air services. The result became the Avioane Craiova IAR-93 Vultur ("Vulture"), an streamlined, high-winged subsonic fighter with modern implements throughout. First flight was recorded on October 31st, 1974 with the line officially introduced during 1979. Manufactured totaled 88 examples and these served with the Romanian Air Force into April of 1998 before it was formally retired from service. Yugoslavia knew the aircraft as the Soko J-22 "Orao" ("Eagle") and was slightly modified to suit local requirements. These were introduced during 1978 and maintain an active status in the Serbian Air Force today (2014) though in limited numbers.

While never seeing combat, the IAR-93's history was noted for its many losses - at least nine - due to various circumstances including mechanical failures and pilot error. At least fifteen went on to live out their days as permanent displays. The project was born as the "Yurom" and saw single-seat and two-seat forms emerge. Both Romania and Yugoslavia undertook construction of their own prototypes for testing.
Engineers elected for a shoulder-wing approach which aided in low-level flight while also offered clear access to underwing hardpoints. The cockpit sat under a largely unobstructed canopy though the view to the rear was blocked by the raised fuselage spine. The nose cone was relatively short and airbrakes featured just aft of the cockpit floor along the ventral side of the fuselage. Internal guns were seated at the lower sides of the forward fuselage for short-range work. Rectangular intakes were affixed to either side of the cockpit walls to aspirate the twin-engine arrangement within. The wing mainplanes were well-swept with dorsal fences added for stability and a pair of hardpoints were featured under each wing. The tail unit was made up of a single vertical tail fin with low-set horizontal planes. The undercarriage was retractable and included a single-wheeled nose leg and a pair of twin-wheeled main legs. Rough-field operations was another key consideration of the type's design.

As a ground attack platform, the aircraft was given an inherent capability to carry, and release, various guided and unguided munitions including missiles, rockets, and unguided drop bombs across its five hardpoints (four underwing, one underfuselage). The aircraft could also take on a low-level interceptor role and, for this, 2 x 23mm GSh-23L twin-barreled cannons were implemented as was support for various existing Soviet-originated Air-to-Air Missiles (AAMs) including the AA-2 "Atoll" and AA-8 "Aphid" types.

There were three major variants of the Vulture produced led by the initial IAR-93A model. The IAR-93A series was given the Viper Mk 632-41 afterburning turbojet engine with manufacture seeing 15 preproduction and 35 production forms emerging (26 as single-seaters and 9 as dual-control, two-seaters). First deliveries were in 1979 with formal service beginning in 1981. Then followed fifteen of the single-seat IAR-93MB during 1982 which installed non-afterburning Viper turbojets.

In 1985, a revised mark appeared in prototype form with Viper Mk 633-47 afterburning engines. The wings were of an all-new design and various protrusions about the fuselage removed for a more streamlined, aerodynamically-refined design form. Thirty-four total aircraft made up this mark, which was introduced in 1987 as the IAR-93B, and included 27 single-seaters and 7 dual-control twin-seaters.

As completed, the IAR-93B version featured a length of 48.9 feet, a wingspan of 30.5 feet, and a height of 14.9 feet. Its empty weight was 12,675lbs with a Maximum Take-Off Weight reaching 22,030lbs. Power was served through 2 x Turbomecanica/Orao (Rolls-Royce) "Viper" Mk 644-47 turbojet engines supplying 4,000lbs of dry thrust and 5,000lbs of power with afterburner engaged. Maximum speed reached 680 miles per hour with a cruising speed closer to 675 miles per hour. Range was 825 miles with a rate-of-climb being 3,900 feet per minute up to a service ceiling of 44,600 feet.

Production of all marks spanned from 1975 into 1992.
Avioane IAR 93B Vultur (Vulture) Specifications
National Flag Graphic
Romania
Year: 1979
Type: Light Strike / Low Altitude Interceptor Aircraft
Manufacturer(s): Avioane Craiova - Romania
Production: 88
Supported Mission Types
Air-to-Air
Interception
Unmanned
Ground Attack
Close-Air Support
Training
Anti-Submarine
Anti-Ship
Airborne Early Warning
MEDEVAC
Electronic Warfare
Maritime/Navy
Aerial Tanker
Utility/Transport
Passenger Industry
VIP Travel
Business Travel
Search/Rescue
Recon/Scouting
Special Forces
X-Plane/Development
Structural
Crew: 1 or 2
Length: 49.21 ft (15 m)
Width: 30.51 ft (9.30 m)
Height: 14.76 ft (4.50 m)
Empty Weight: 12,677 lb (5,750 kg)
MTOW: 24,030 lb (10,900 kg)


Installed Power
2 x Orao-Turbomecanica (Rolls-Royce) Viper Mk 533-47 afterburning turbojet engines developing 5,000lbs thrust each.

Standard Day Performance
Maximum Speed: 677 mph (1,090 kph; 589 kts)
Maximum Range: 820 mi (1,320 km; 713 nm)
Service Ceiling: 44,619 ft (13,600 m; 8.45 mi)
Rate-of-Climb: 12,800 ft/min (3,901 m/min)


Armament
STANDARD:
2 x 23mm GSh-23L internal cannons

OPTIONAL:
Up to 5,500lbs of external stores to include support for guided missiles, laser-guided bombs, conventional drop bombs, rocket pods, cannon pods and gun pods.


Operators List
Romania

Series Model Variants
• IAR 93A - Initial Production Models with non-afterburning engines.
• IAR 93B - Afterburning engines
• IAR 93MB - Non-afterburning engines with fuselage of A-models.


Supported Weapon Systems
Graphical image of an aircrat automatic cannon
Graphical image of an aircraft machine gun pod
Graphical image of an aircraft cannon pod
Graphical image of an aircraft rocket pod
Graphical image of an aircraft conventional drop bomb munition
Graphical image of an aircraft guided bomb munition