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- JF-17 Thunder vs Rafale: Which Fighter Jet Wins in 2026? Full Specs Comparison
JF-17 Thunder vs Rafale: Which Fighter Jet Wins in 2026? Full Specs Comparison
The JF-17 Thunder and Dassault Rafale represent two distinct philosophies in modern fighter jet design. The JF-17 Thunder, a lightweight single-engine multirole fighter jointly developed by Pakistan and China, serves as an affordable, versatile platform for the Pakistan Air Force. Priced around $25-30 million per unit, it features a top speed of Mach 1.6, KLJ-7A AESA radar in newer blocks, and a payload of up to 3,700 kg, making it ideal for cost-effective air defense and ground attack missions.
General Information
|
Name
|
JF-17 Thunder / FC-1 Xiaolong
Dassault Rafale |
|
Manufacturer
|
Pakistan Aeronautical Complex (PAC) & Chengdu Aircraft Industry Group (CAIG)
Dassault Aviation |
|
Country of Origin
|
Pakistan / China
France |
|
Type / Role
|
Multirole Fighter
Multirole Fighter |
|
Generation
|
4.5th
4.5th |
|
Status
|
Active Service
Active Service |
|
First Flight
|
August 25, 2003
July 4, 1986 |
|
Introduction / In Service Since
|
2010
2001 |
|
Number Built
|
175+ units
240+ |
|
Operators
|
Pakistan, Myanmar, Nigeria, Azerbaijan
France, India, Egypt, Qatar, Greece, Indonesia |
Dimensions & Structure
|
Length
|
14.33 m (47 ft)
15.27 m |
|
Wingspan
|
9.44 m (31 ft)
10.9 m |
|
Height
|
4.57 m (15 ft)
5.3 m |
|
Wing Area
|
24.4 m² (263 sq ft)
45.7 m² |
|
Empty Weight
|
6,586 kg (14,520 lbs)
10,600 kg |
|
Maximum Takeoff Weight (MTOW)
|
13,500 kg (29,762 lbs)
24,500 kg |
|
Internal Weapons Bay
|
None
None |
|
External Hardpoints
|
8 (including wingtip rails)
14 |
Performance
|
Maximum Speed
|
Mach 1.8 (1,910 km/h / 1,187 mph)
Mach 1.8 (2,223 km/h) |
|
Range
|
3,482 km (2,164 mi) with external drop tanks
3,700 km |
|
Combat Radius
|
900 km (560 mi) on internal fuel
1,000–1,850 km |
|
Service Ceiling
|
16,916 m (55,500 ft)
50,000 ft |
|
Rate of Climb
|
300 m/s (59,000 ft/min)
305 m/s |
|
Thrust-to-Weight Ratio
|
1.07 (with full afterburner)
1.13 |
|
G Limits
|
+8 / -3
+9 / -3.6 |
Powerplant
|
Engine Type
|
Klimov RD-93MA afterburning turbofan
Snecma M88-2 Turbofan |
|
No. of Engines
|
1
2 |
|
Thrust (each)
|
50.4 kN dry / 91.2 kN with afterburner
16,500 lbf |
|
Thrust Vectoring
|
No
No |
|
Fuel Capacity
|
2,268 kg (5,000 lbs) internal
4,700 kg (internal) |
Armament
|
Gun
|
1 × 23 mm GSh-23-2 twin-barrel autocannon
GIAT 30mm cannon |
|
Missiles (Air-to-Air)
|
PL-5E, PL-10, PL-12, PL-15E (BVR)
MICA, Meteor |
|
Missiles (Air-to-Ground)
|
Ra'ad ALCM, CM-400AKG, C-802AK Anti-Ship
SCALP-EG, AM39 Exocet |
|
Bombs
|
LT-2 (Laser-guided), LS-6 (GPS-guided), Mk-82/84
Paveway, AASM |
|
Hardpoints
|
8
14 |
|
Payload Capacity
|
3,600 kg (7,936 lbs)
9,500 kg |
Avionics & Systems
|
Radar
|
KLJ-7A Active Electronically Scanned Array (AESA)
Thales RBE2 AESA |
|
Radar Range
|
160–170 km (against fighter-sized target)
200+ km |
|
Electronic Warfare (EW) System
|
Integrated digital EW suite & Missile Approach Warning System
SPECTRA Suite |
|
Targeting System
|
Aselsan ASELPOD / WMD-7 targeting pods
Thales Damocles / TALIOS Pod |
|
Helmet Display
|
Helmet-Mounted Display and Sight (HMD/S)
Integrated HMD |
|
Navigation
|
INS + GPS/Beidou satellite navigation
GPS/INS |
|
Autopilot / AI Assistance
|
Three-axis digital Fly-By-Wire (FBW) system
Semi-Automated |
|
Communication
|
Secure, jam-resistant tactical data link
Secure Datalink, SATCOM |
Stealth & Technology
|
Radar Cross Section (RCS)
|
Reduced frontal RCS compared to older blocks
~1 m² |
|
Stealth Features
|
Radar-absorbent material coatings & minor airframe shaping
Radar-absorbent materials |
|
Infrared Signature Reduction
|
Limited
Yes |
|
Sensor Fusion
|
Partial multi-sensor architecture
Full |
|
Networking Capabilities
|
Real-time command data sharing with ground/AWACS
NATO-compatible datalink |
Variants
|
Special Export Versions
|
JF-17N (Nigeria) – customized avionics and weapon suite; JF-17M (Myanmar) – tailored for local integration; JF-17E (Export) – export-optimized with optional Western avionics and weapon compatibility.
Rafale EH/IH (India), Rafale EM/QM (Egypt/Qatar) |
Operational History
|
Major Conflicts / Deployments
|
Operation Swift Retort (2019), Counter-insurgency ops
Libya, Mali, Iraq, Syria |
|
Notable Operators
|
Pakistan Air Force, Azerbaijan Air Force
France, India, Egypt |
|
Combat Proven?
|
Yes
Yes |
|
Mission Types
|
Air Defense, Interdiction, Close Air Support, Anti-Ship Strike
Air superiority, strike, reconnaissance, deterrence |
Cost & Program
|
Unit Cost
|
$25 million – $35 million (estimated variant dependent)
$85–115 million |
|
Development Cost
|
$500 million (jointly shared initial program)
~$45 billion |
|
Program Name
|
Super-7 / JF-17 Thunder Program
Rafale Program |
|
Funding Countries
|
Pakistan and China
France |
Additional Information
|
Upgrades Planned
|
Enhanced software integration and localized missile adaptations.
F4 & F5 standard upgrades |
|
Future Replacement
|
Project AZM Next-Gen Fighter / Fifth-Gen acquisitions.
Next-Gen Fighter (FCAS) |
|
Export Restrictions
|
Subject to joint approval by Pakistan and China.
Minimal (case-by-case) |
|
Notable Achievements
|
Successful integration of true long-range PL-15E BVR system.
Combat-proven multirole success |
|
Competitors
|
HAL Tejas (India), JAS 39 Gripen (Sweden), F-16 Fighting Falcon (USA)
Eurofighter Typhoon, F/A-18E/F, Gripen E |
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