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  4. JF-17 Thunder vs J-10C Fighter Jet: Detailed Comparison, Specs & Which is Better?

JF-17 Thunder vs J-10C Fighter Jet: Detailed Comparison, Specs & Which is Better?

The JF-17 Thunder and Chengdu J-10C represent two formidable single-engine multirole fighters from the China-Pakistan collaboration and Chinese aviation industry. The JF-17 Thunder (also known as FC-1 Xiaolong), a lightweight supersonic fighter jointly developed by Pakistan Aeronautical Complex and Chengdu Aircraft Corporation, serves as a cost-effective backbone for the Pakistan Air Force. It excels in agility, low operational costs, and versatility for air-to-air and air-to-ground missions.

In contrast, the J-10C “Vigorous Dragon” is a more advanced medium-weight fighter with superior thrust, payload capacity, and avionics, including a powerful AESA radar and WS-10B engine. It offers better speed (up to Mach 1.8-2.2), range, and heavy weaponry like PL-15 BVR missiles, making it suitable for high-threat environments.

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General Information

Name JF-17 Thunder / FC-1 Xiaolong Chengdu J-10C (Vigorous Dragon)
Manufacturer Pakistan Aeronautical Complex (PAC) & Chengdu Aircraft Industry Group (CAIG) Chengdu Aircraft Industry Group (CAIG)
Country of Origin Pakistan / China China
Type / Role Multirole Fighter Multirole Fighter
Generation 4.5th 4.5
Status Active Service In service
First Flight August 25, 2003 2013
Introduction / In Service Since 2010 2018
Number Built 175+ units 200+
Operators Pakistan, Myanmar, Nigeria, Azerbaijan China, Pakistan

Dimensions & Structure

Length 14.33 m (47 ft) 16.9 m
Wingspan 9.44 m (31 ft) 9.8 m
Height 4.57 m (15 ft) 5.4 m
Wing Area 24.4 mยฒ (263 sq ft) 33 mยฒ
Empty Weight 6,586 kg (14,520 lbs) 9,750 kg
Maximum Takeoff Weight (MTOW) 13,500 kg (29,762 lbs) 19,200 kg
Internal Weapons Bay None None
External Hardpoints 8 (including wingtip rails) 11

Performance

Maximum Speed Mach 1.8 (1,910 km/h / 1,187 mph) Mach 2.0
Range 3,482 km (2,164 mi) with external drop tanks 1,850 km
Combat Radius 900 km (560 mi) on internal fuel ~1,000 km
Service Ceiling 16,916 m (55,500 ft) 56,000 ft
Rate of Climb 300 m/s (59,000 ft/min) 60,000 ft/min
Thrust-to-Weight Ratio 1.07 (with full afterburner) 1.1
G Limits +8 / -3 +9

Powerplant

Engine Type Klimov RD-93MA afterburning turbofan WS-10B Taihang Turbofan
No. of Engines 1 1
Thrust (each) 50.4 kN dry / 91.2 kN with afterburner 13,200 kgf (with afterburner)
Thrust Vectoring No Optional variant
Fuel Capacity 2,268 kg (5,000 lbs) internal ~4,500 kg internal

Armament

Gun 1 ร— 23 mm GSh-23-2 twin-barrel autocannon 23mm GSh-23 twin-barrel cannon
Missiles (Air-to-Air) PL-5E, PL-10, PL-12, PL-15E (BVR) PL-10, PL-12, PL-15
Missiles (Air-to-Ground) Ra'ad ALCM, CM-400AKG, C-802AK Anti-Ship KD-88, YJ-91, LT-series
Bombs LT-2 (Laser-guided), LS-6 (GPS-guided), Mk-82/84 LS-6, LT-2 guided bombs
Hardpoints 8 11
Payload Capacity 3,600 kg (7,936 lbs) 6,000 kg

Avionics & Systems

Radar KLJ-7A Active Electronically Scanned Array (AESA) KLJ-7A AESA
Radar Range 160โ€“170 km (against fighter-sized target) ~170 km
Electronic Warfare (EW) System Integrated digital EW suite & Missile Approach Warning System ECM suite with radar warning receiver
Targeting System Aselsan ASELPOD / WMD-7 targeting pods Electro-optical/laser pod
Helmet Display Helmet-Mounted Display and Sight (HMD/S) Yes
Navigation INS + GPS/Beidou satellite navigation INS/GPS hybrid
Autopilot / AI Assistance Three-axis digital Fly-By-Wire (FBW) system Fly-by-wire with limited AI assist
Communication Secure, jam-resistant tactical data link Data link with PLAAF C4ISR network

Stealth & Technology

Radar Cross Section (RCS) Reduced frontal RCS compared to older blocks ~1.0 mยฒ (reduced)
Stealth Features Radar-absorbent material coatings & minor airframe shaping RAM coatings, intake shaping
Infrared Signature Reduction Limited Partial exhaust masking
Sensor Fusion Partial multi-sensor architecture Integrated data fusion
Networking Capabilities Real-time command data sharing with ground/AWACS Compatible with KJ-500 AEW&C systems

Variants

Special Export Versions JF-17N (Nigeria) โ€“ customized avionics and weapon suite; JF-17M (Myanmar) โ€“ tailored for local integration; JF-17E (Export) โ€“ export-optimized with optional Western avionics and weapon compatibility. J-10CE (Pakistan)

Operational History

Major Conflicts / Deployments Operation Swift Retort (2019), Counter-insurgency ops None (peacetime operations)
Notable Operators Pakistan Air Force, Azerbaijan Air Force PLAAF, Pakistan Air Force
Combat Proven? Yes Not yet
Mission Types Air Defense, Interdiction, Close Air Support, Anti-Ship Strike Air superiority, strike, interception

Cost & Program

Unit Cost $25 million โ€“ $35 million (estimated variant dependent) ~$35โ€“40 million
Development Cost $500 million (jointly shared initial program) Classified
Program Name Super-7 / JF-17 Thunder Program J-10 Development Program
Funding Countries Pakistan and China China

Additional Information

Upgrades Planned Enhanced software integration and localized missile adaptations. WS-15E engine, enhanced EW suite
Future Replacement Project AZM Next-Gen Fighter / Fifth-Gen acquisitions. Sixth-generation Chinese fighter
Export Restrictions Subject to joint approval by Pakistan and China. Moderate (friendly nations only)
Notable Achievements Successful integration of true long-range PL-15E BVR system. First PLAAF jet with AESA radar
Competitors HAL Tejas (India), JAS 39 Gripen (Sweden), F-16 Fighting Falcon (USA) F-16V, Rafale, Gripen E
  JF-17 Thunder Fighter Jet Chengdu J-10C Fighter Jet

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