el j-10 fue un avion chino diseñado para "contrarrestar" a los su-27 y a los mig-29 sovieticos en plena guerra fria J-10 Specifications
HISTORY
First flight 24 March 1998
Initial operational capability 2003
Operator PLA Air Force
Variants J-10 (prototype)
J-10A (single-seat fighter)
J-10B (two-seat fighter-trainer)
CREW
J-10A One
J-10B Two
DESIGN
Role Air-superiority, ground attack
Designer 611 Aircraft Design Institute, Chengdu
Manufacturer Chengdu Aircraft Company
Estimated cost N/A
DIMENSIONS
Length N/A
Wingspan N/A
Height N/A
Wing area N/A
Canard area N/A
WEIGHTS
Empty N/A
Typical load N/A
Max take-off N/A
Fuel capacity N/A
Max payload N/A
PROPULSION
Powerplant 1X Russian Lyulka-Saturn AL-31F turbofan
Thrust (dry) 79.43kN (17,857lb)
Thrust (afterburning) 122.58kN (27,557lb)
PERFORMANCE
Max level speed Mach 1.2 (sea-level) or Mach 2.0 (high altitude)
Max climb rate N/A
Service ceiling N/A
Range (without refuelling) >1,300km
In-flight refuelling Yes
G limit +9
ARMAMENTS
Fixed weapon Single-barrel 23mm internal cannon
External hardpoints 11
Air-to-air missiles PL-8, PL-12
Air-to-surface missiles N/A
Bomb 500kg laser-guided bomb
Other 90mm unguided rocket launcher
AVIONICS
Fire-control radar Unknown model, 100km+ detecting range, multi-target tracking
Other ‘glass cockpit’ with three multifunctional displays (MFD) (one colour and two monochrome), wide-angle head-up display (HUD), GPS/INS navigations, air data computer, ARW9101 radar warning receiver (RWR), Type 634 digital quadruplex “fly-by-wire” (FBW) system, and digital fuel management system
ahi tenes no se ingles lo copie de aca
http://www.sinodefence.com/airforce/fighter/j10specifications.asp