Xi'an JH-7 - Fotos & Videos

Xi’an JH-7
Land	People’s Republik China
Rolle	Jagdbomber
Erstflug	14. Dezember 1988
Gebaut	270+

Die Xi'an JH-7 (Jianjiji Hongzhaji – Jagdbomber; Der NATO-Codename Flunder), auch bekannt als FBC-1 (Fighter/Bomber China-1) Flying Leopard, ist ein zweisitziger, zweimotoriger Jagdbomber im Dienst der People's Liberation Army Naval Air Force (PLANAF) und der People's Liberation Army Air Force (PLAAF). Die Hauptauftragnehmer sind die Xi'an Aircraft Industrial Corporation (XAC) und das 603rd Aircraft Design Institute (später First Aircraft Institute of AVIC-I genannt).

Quelle: Xi'an JH-7 auf Wikipedia

JH 7A Flying Leopard Walk Around
Fotograf	Unknow
Lokalisierung	Unbekannter
Fotos	19

JH 7A Flying Leopard 01

JH 7A Flying Leopard 02

JH 7A Flying Leopard 03

JH 7A Flying Leopard 04

JH 7A Flying Leopard 05

JH 7A Flying Leopard 06

JH 7A Flying Leopard 07

JH 7A Flying Leopard 08

JH 7A Flying Leopard 09

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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)
Rolle	Fighter-Bomber / Maritime Strike Aircraft
National Origin	China (PRC)
Hersteller	Xian Aircraft Industrial Corporation (XAC)
Service Entry (JH-7A)	c. 2004
Crew	2 (Pilot, Weapon System Operator)
Length (Total)	22.33 m (73 ft 3 in)
Flügelspannweite	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.