Length
13.6 m
Flat Wing Span
9.5 m
Height
4.1 m
Flat Wing Area
25 m²
Max Mach
1.4 Mach
Max Ceiling
14000 m
Number of Engines
1
Aircraft Engine
First Flight
2023-04-25
Entry Into service
2026-01-01
Number Built
1
Maximum Range
1960 km

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Aircraft Maximum Range (km)
TAI Hürjet 1960

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All data (22 fields)
Name
TAI Hürjet
Manufacturer
Turkish Aerospace Industries
Description
The TAI Hürjet is a single-engine, tandem seat, supersonic advanced jet trainer and light combat aircraft, under development by Turkish Aerospace Industries (TAI).
First Flight
2023-04-25
Entry Into service
2026-01-01
Designer
Turkish Aerospace Industries
Length (m)
13.6
Height (m)
4.1
Cockpit Crew
2
Max Ceiling (m)
14000
Rate of Climb (m/s)
246
Armament
Hardpoints: Provision for a total of seven pylon stations (one × under-fuselage, four × under-wing plus two × wingtip)
Max Mach (Mach)
1.4
National Origin
Turkey
Number Built
1
Powerplant Description
1 × General Electric F404-GE-104 afterburning turbofan engine, 53.07 kN thrust each
Status
Scheduled to enter operational service
Wikipedia Article (URL)
en.wikipedia.org/wiki/TAI_H%C3%BCrjet
Flat Wing Span (m)
9.5
Flat Wing Area (m²)
25
Aircraft Engine
General Electric F404
Number of Engines
1