Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Shenyang J-13 Air Superiority Fighter Project.
1 x Woshan WS-6 OR WP-15 turbofan engine developing at least 26,455lb of thrust with afterburning.
Propulsion
1,880 mph
3,025 kph | 1,633 kts
Max Speed
62,336 ft
19,000 m | 12 miles
Service Ceiling
1,454 miles
2,340 km | 1,263 nm
Operational Range
40,000 ft/min
12,192 m/min
Rate-of-Climb