Credit
Alan Wilson · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
G 115E · Length
Single source7.79 m (25 ft 7 in)[source]
Yak-130 · Length
Single sourceConfiguration
| Specification | Grob G 115 | Yakovlev Yak-130 |
|---|---|---|
| Type | Basic trainer[source] | Lead-in fighter trainer / Light combat aircraft[source] |
| Manufacturer | Grob Aircraft[source] | Yakovlev, Sokol, Yakovlev Corporation[source] |
| Status | active[source] | Active[source] |
| Primary users | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] | Russian Aerospace Forces Bangladesh Air Force Algerian Air Force Myanmar Air Force Islamic Republic of Iran Air Force |
11.49 m (37 ft 8 in)[source]
Cruise; G 115E · long range cruising speed
Single sourceMaximum; G 115E · Maximum speed
Single source250 km/h (160 mph, 130 kn)[source]
178 km/h (111 mph, 96 kn) (long range cruising speed)[source]
Cruise; Yak-130 · Cruise speed
Single sourceMaximum; Yak-130 · Maximum speed
Single sourceG 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]
Yak-130 · 2 × Ivchenko-Progress AI-222-25 turbofan engines thrust each
Single source2 × Ivchenko-Progress AI-222-25 turbofan engines, 24.52 kN (5,510 lbf) thrust each[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] | 19 February 2010[source] |
|---|
| First flight | November 1985[source] | 25 April 1996 ( 1996-04-25 ) (Yak/AEM-130) 30 April 2004 ( 2004-04-30 ) (Yak-130)[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] | 165 km/h (103 mph, 89 kn)[source] |
|---|
| Never exceed speed | 341 km/h (212 mph, 184 kn)[source] | — |
|---|
| g limits | + 6.0/ - 3.0[source] | + 8.0 − 3.0[source] |
|---|
| Country of origin | Deutschland[source]Country of design · Entwurfsland | — |
|---|
| National origin | — | Russia[source] |
|---|
| Designer | — | Yakovlev[source] |
|---|
| Built by | — | Irkut Corporation Sokol Aircraft Plant[source] |
|---|
| Number built | — | 219[source] |
|---|
| Variant | — | Alenia Aermacchi M-346 Master[source] |
|---|
| Guns | — | SNPU-130 gun pod[source] |
|---|
| Hardpoints | — | 8 (1 on each wingtip, usable only for flares/chaff, 3 under each wing) with a capacity of up to 3,000 kg (6,614 lb), with provisions to carry combinations of: Rockets: 80 mm S-8 rocket, S-25 rocket Missiles: R-73 infrared-homing short-range air-to-air missiles Bombs: FAB-M62, ZB-500, KAB-500Kr[source] |
|---|
| Wing loading | — | 276.4 kg/m 2 (56.6 lb/sq ft)[source] |
|---|
| Thrust/weight | — | 0.70[source] |
|---|
| Rockets | — | 80 mm S-8 rocket, S-25 rocket[source] |
|---|
| Missiles | — | R-73 infrared-homing short-range air-to-air missiles[source] |
|---|
| Bombs | — | FAB-M62, ZB-500, KAB-500Kr[source] |
|---|
| Alternative designation | — | Yak-130[source] |
|---|
Maximum take-off; Yak-130 · Max takeoff weight
Single source