(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the PZL TS-11 Iskra-bis D production variant)
1 x WSK SO-3 turbojet engine developing 2,205 lb of thrust.
(720 kph | 389 kts)
(11,000 m | 7 mi)
(1,250 km | 2,315 nm)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
(Showcased performance specifications pertain to the PZL TS-11 Iskra-bis D production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
1 x 23mm NS-23 / NR-23 cannon in nose.
Up to 880lb of externally-carried stores including conventional drop bombs, rocket pods, and cannon pods.
(Not all ordnance types may be represented in the showcase above)
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.