Soko J-22 Orao | |
|---|---|
| 국가 | 루마니아 & 유고슬라비아 |
| 역할 | Attack aircraft & Reconnaissance aircraft |
| 첫 비행 | 1974년 10월 31일 |
| 내장 | Unknow |
Tthe 소코 J-22 오라오 유고 슬라비아 쌍발 엔진, 아음속 지상 공격 및 공중 정찰기입니다. 유고슬라비아의 SOKO와 이웃 루마니아의 Avioane Craiova가 공동으로 개발 및 제작했으며, 후자에서는 IAR-93 Vultur로 알려져 있습니다.
| 소코 J-22 오라오 | |
|---|---|
| 사진 작가 | Unknow |
| 로컬라이제이션 | Unknow |
| 사진 | 80 |
Soko J-22 Orao 11
Soko J-22 Orao 13
Soko J-22 Orao 12
Soko J-22 Orao 14
Soko J-22 Orao 15
Soko J-22 Orao 16
Soko J-22 Orao 17
Soko J-22 Orao 18
Soko J-22 Orao 19
대기,검색 소코 J-22 오라오 당신을 위해...
커피 사줘
참고 항목:
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) |
|---|---|
| 역할 | Ground Attack / Tactical Reconnaissance |
| 제조업체 | SOKO (Yugoslavia) / Avioane Craiova (Romania) |
| First Flight | November 1974 |
| 승무원 | 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) |
| 윙스 팬 | 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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