Credit
Alan Wilson · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
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BTrainer aircraft
Advanced jet trainer ( lead-in fighter trainer ) and Light combat aircraft
At a glance
Measured figures
G 115E · Length
Single source7.79 m (25 ft 7 in)[source]
Length
Single sourceConfiguration
| Specification | Grob G 115 | TAI Hürjet |
|---|---|---|
| Type | Basic trainer[source] | Advanced jet trainer ( lead-in fighter trainer ) and Light combat aircraft[source] |
| Manufacturer | Grob Aircraft[source] | Turkish Aerospace Industries[source] |
| Status | active[source] | Scheduled to enter operational service[source] |
| Primary users | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] | — |
13.6 m (44 ft 9 in)[source]
G 115E · 1 × Lycoming AEIO-360-B1F/B 4-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming AEIO-360-B1F/B 4-cylinder air-cooled horizontally-opposed piston engine, 130 kW (180 hp)[source]
1 × General Electric F404 -GE-104 afterburning turbofan engine thrust dry
Single sourcewith afterburner
Single source1 × General Electric F404 -GE-104 afterburning turbofan engine, 53.07 kN (11,930 lbf) thrust dry, 78.7 kN (17,700 lbf) with afterburner[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1985–present[source] | — |
|---|
| Introduction date | 1999[source] | 2026[source] |
|---|
| First flight | November 1985[source] | 25 April 2023[source] |
|---|
| Fuel capacity | 143 L (31 imp gal; 38 US gal) usable[source] | — |
|---|
| Aspect ratio | 8.2:1[source] | — |
|---|
| Airfoil | Eppler 696[source] | — |
|---|
| Propellers | 3-bladed Hoffmann HO-V343K-V/183GY Constant-speed propeller , 1.83 m (6 ft 0 in) diameter[source] | — |
|---|
| Stall speed | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] | — |
|---|
| Never exceed speed | 341 km/h (212 mph, 184 kn)[source] | — |
|---|
| g limits | + 6.0/ - 3.0[source] | + 8 − 3[source] |
|---|
| Country of origin | Deutschland[source]Country of design · Entwurfsland | — |
|---|
| National origin | — | Turkey[source] |
|---|
| Prototypes | — | 3 prototypes[source] |
|---|
| Number built | — |
|---|
| Hardpoints | — | Provision for a total of seven pylon stations (one × under-fuselage, four × under-wing plus two × wingtip)[source] |
|---|