PZL TS-11 Iskra

· PZL Mielec

Airplanes

Length

11.15 m

Flat Wing Span

10.06 m

Height

3.5 m

Flat Wing Area

17.5 m²

Cruise Speed

600 km/h

Max Speed

720 km/h

Max Ceiling

11000 m

Number of Engines

First Flight

1960-02-05

Entry Into service

1964-01-01

Number Built

424

Maximum Take-Off Weight

3.84 t (paragliders: kg)

Maximum Range

1250 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
PZL TS-11 Iskra	3.84	1250

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
A Vlaicu II	Gnome Omega	11.2	10	Compare
TAI Hürkuş	Pratt & Whitney Canada PT6	11.17	9.96	Compare
IAR 99		11.01	9.85	Compare
Vought F6U Pirate	Westinghouse J34	11.46	10	Compare
A Vlaicu III	Gnome Gamma	10.75	10	Compare
Shenyang J-5		11.09	9.628	Compare

All data (28 fields)

Name: PZL TS-11 Iskra
Manufacturer: PZL Mielec
Description: The PZL TS-11 Iskra () is a Polish jet trainer, developed and manufactured by aircraft company PZL-Mielec.
ICAO Code: TS11
First Flight: 1960-02-05
Entry Into service: 1964-01-01
Production End: 1987-01-01
Service End: 2021-01-01
Designer: PZL Mielec
Type: Trainer aircraft
Length (m): 11.15
Height (m): 3.5
Cockpit Crew: 2
Max Speed (km/h): 720
Cruise Speed (km/h): 600
Min Speed (km/h): 140
Max Ceiling (m): 11000
Rate of Climb (m/s): 14.8
Armament: 1x 23 mm NS-23 or NR-23 cannon in the nose; 4 underwing pylons, up to 400 kg (880 lb) of bombs or unguided S-5 rocket pods Mars-4 (8 rockets) or Zeus-1 (12,7mm) gun packs.
Number Built: 424
Powerplant Description: 1 × WSK SO-3 turbojet engine, 9.81 kN thrust each
Primary Users: Polish Air Force, Polish Navy , Indian Air Force
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/PZL_TS-11_Iskra
Flat Wing Span (m): 10.06
Flat Wing Area (m²): 17.5
Wake Category: L
Number of Engines: 1