Soko J-22 Orao | |
|---|---|
| Land | Romania og Jugoslavia |
| Rolle | Angrepsfly og rekognoseringsfly |
| Første flytur | 31. oktober 1974 |
| Bygget | Unknow |
Den Soko J-22 Orao er et jugoslavisk tomotors, subsonisk bakkeangrep og luftrekognoseringsfly. Den ble utviklet og bygget i samarbeid mellom SOKO i Jugoslavia og av Avioane Craiova i nabolandet Romania, kjent i sistnevnte som IAR-93 Vultur.
Kilde: Soko J-22 Orao på Wikipedia
| Soko J-22 Orao | |
|---|---|
| Fotograf | Unknow |
| Lokalisering | Unknow |
| Bilder | 80 |
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General Characteristics (J-22B Orao 2 Variant)
The Soko J-22 Orao (“Eagle”) is a twin-engine, high-wing, subsonic ground-attack and tactical reconnaissance aircraft developed as a joint Yugoslav-Romanian project (known in Romania as the IAR-93 Vultur). Designed for close air support and attack missions, it was built to be robust, simple, and capable of operating from austere airfields, including unprepared and damaged runways.
| Property | Typical Value (J-22B Orao 2) |
|---|---|
| Rolle | Ground Attack / Tactical Reconnaissance |
| Produsenten | SOKO (Yugoslavia) / Avioane Craiova (Romania) |
| First Flight | November 1974 |
| Mannskapet | 1 (J-22 single-seat attack) or 2 (NJ-22 two-seat trainer/reconnaissance) |
| Length (including nose probe) | 14.90 m (48 ft 11 in) |
| Vingespenn | 9.30 m (30 ft 6 in) |
| Max Takeoff Weight | 11,080 kg (24,427 lb) |
Design and Powerplant
- Engines: Two Rolls-Royce Viper Mk 633-47 turbojet engines (Orao/Turbomecanica license-built).
- Thrust Output (per engine): 17.79 kN (4,000 lbf) dry; 22.24 kN (5,000 lbf) with afterburner (on J-22B variant).
- Design Note: The original requirement called for a single-engine supersonic aircraft, but due to engine license restrictions, the simpler, subsonic twin-Viper configuration was adopted. The J-22 can exceed the speed of sound only in a shallow dive.
- Cockpit: Equipped with a Martin-Baker zero-zero ejection seat and features a Thomson-CSF VE-120T Head-Up Display (HUD) in later versions.
- Maintenance Feature: The rear fuselage section is designed to be detachable to facilitate easy engine maintenance.
- Avionics: Later modernization efforts (Orao 2.0) included new mission computers, multi-function displays, and integrated navigation/targeting systems.
Performance and Armament
- Maximum Speed: 1,130 km/h (700 mph, 610 kn) at sea level (Mach 0.96 at high altitude).
- Service Ceiling: 15,000 m (49,000 ft).
- Combat Radius: Approximately 522 km (282 nautical miles) (hi-lo-hi profile).
- Ferry Range: Approximately 1,320 km (710 nautical miles) with external drop tanks.
- Fixed Armament: Two 23 mm GSh-23L twin-barrel cannons mounted in the lower front fuselage.
- Hardpoints: Five external hardpoints (four underwing and one centerline).
- Maximum External Load: 2,800 kg (6,200 lb).
- Typical Armament Options:
- Missiles: AGM-65B Maverick TV-guided Air-to-Ground Missiles (AGM) or Grom-1 radio-guided AGMs.
- Bombs: Various 50–500 kg general-purpose bombs, cluster bombs (BL755), and anti-runway bombs (Matra Durandal).
- Rockets: Multiple types of unguided rocket pods.
- Air-to-Air: Limited air defense capability using short-range IR-homing air-to-air missiles on later variants.
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