
Xi’an JH-7 | |
|---|---|
| País | República Popular China |
| Papel | Cazabombarderos |
| Primer vuelo | 14 de diciembre de 1988 |
| Construido | 270+ |
El Xi'an JH-7 (Jianjiji Hongzhaji – cazabombardero; El nombre de informe de la OTAN Flounder), también conocido como FBC-1 (Fighter/Bomber China-1) Flying Leopard, es un cazabombardero bimotor biplaza en tándem en servicio con la Fuerza Aérea Naval del Ejército Popular de Liberación (PLANAF) y la Fuerza Aérea del Ejército Popular de Liberación (PLAAF). Los principales contratistas son Xi'an Aircraft Industrial Corporation (XAC) y el 603rd Aircraft Design Institute (más tarde llamado First Aircraft Institute of AVIC-I).
Fuente: Xi'an JH-7 en Wikipedia
| JH 7A Flying Leopard Walk Around | |
|---|---|
| Fotógrafo | Unknow |
| Localización | Unknow |
| Fotos | 19 |
Ver también:
General Characteristics
The Xian JH-7 (Jian Hong – Fighter Bomber), nicknamed the Flying Leopard (NATO reporting name: Flounder), is a Chinese twin-engine, tandem two-seat fighter-bomber. The JH-7A is the majorly upgraded, fully digitized production variant that entered service in the mid-2000s, serving as a primary platform for deep strike, ground attack, and maritime strike missions for both the People’s Liberation Army Air Force and Naval Air Force. The JH-7A features an improved airframe using more composite materials, a single-piece windscreen, and a digital fly-by-wire flight control system, significantly enhancing its combat capabilities over the original JH-7.
| Property | Typical Value (JH-7A) |
|---|---|
| Papel | Fighter-Bomber / Maritime Strike Aircraft |
| National Origin | China (PRC) |
| Fabricante | Xian Aircraft Industrial Corporation (XAC) |
| Service Entry (JH-7A) | c. 2004 |
| Equipo | 2 (Pilot, Weapon System Operator) |
| Length (Total) | 22.33 m (73 ft 3 in) |
| Envergadura | 12.71 m (41 ft 8 in) |
| Max Takeoff Weight | 30,000 kg (66,139 lb) |
Powerplant and Performance
- Engine: 2 x Xian WS-9 (Chinese license-built version of the Rolls-Royce Spey Mk 202) turbofan engines.
- Max Thrust (per engine, w/ afterburner): 91.2 kN (20,515 lbf).
- Maximum Speed: Mach 1.7 (Approx. 2,081 km/h or 1,293 mph).
- Service Ceiling: 15,600 m (51,180 ft).
- Combat Radius: Approx. 1,650 km (1,025 mi).
- Ferry Range: Approx. 3,650 km (2,268 mi).
- G-Limit: +7 g.
Armament and Avionics
- Internal Gun: 1 x 23 mm GSh-23L twin-barrel autocannon (300 rounds).
- Hardpoints: 9 total (6 under-wing, 2 under-intake for pods, 1 centerline) + 2 wingtip rails for Air-to-Air Missiles.
- Max Ordnance Load: 9,000 kg (20,000 lb).
- Key Munitions:
- Anti-Ship Missiles (ASMs): YJ-83K, YJ-81, C-802K (for naval targets).
- Air-to-Surface Missiles (ASMs): KD-88, Kh-29 (for land targets).
- Anti-Radiation Missiles (ARMs): YJ-91, LD-10 (for SEAD missions).
- Guided Bombs: LS, LT, FT, and GB series laser and satellite-guided bombs.
- Air-to-Air Missiles (AAMs): PL-5, PL-8, PL-9 (for self-defense).
- Avionics & Sensors (JH-7A):
- Radar: JL-10A pulse-Doppler radar (multimode with look-down/shoot-down capability).
- Cockpit: Two large color Multi-Function Displays (MFDs).
- Navigation: Integrated Inertial Navigation System/Global Positioning System (INS/GPS).
- Targeting: Can carry external targeting pods (e.g., Blue Sky low-altitude navigation pod) and is compatible with a Helmet Mounted Sight (HMS).
- ECM/EW: Features a comprehensive Electronic Countermeasures (ECM) suite, Radar Warning Receiver (RWR), and chaff/flare dispensers.
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