Credit
Tim Felce (Airwolfhound) · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Hawk 128 · Length
Single source12.43 m (40 ft 9 in)[source]
G 115E · Length
Single sourceConfiguration
| Specification | BAE Systems Hawk | Grob G 115 |
|---|---|---|
| Type | Advanced trainer aircraft[source] | Basic trainer[source] |
| National origin | United Kingdom[source] | — |
| Manufacturer | Hawker Siddeley (1974–1977) British Aerospace (1977–1999) BAE Systems MAI division (1999–2022) Hindustan Aeronautics Limited (2008–present)[source] | Grob Aircraft[source] |
| Status | In service[source] | active[source] |
7.79 m (25 ft 7 in)[source]
Maximum; Hawk 128 · ) at altitude
Single sourceMaximum; Hawk 128 · Mach 0.84 (
Single sourceMaximum; Hawk 128 · Maximum speed
Single sourceMach 0.84 (1,028 km/h, 639 mph, 555 kn) at altitude[source]
Cruise; G 115E · long range cruising speed
Single sourceMaximum; G 115E · 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]
Hawk 128 · 1× Rolls-Royce Turbomeca Adour Mk. 951 turbofan with FADEC
Single sourceHawk 128 · Powerplant
Single source1× Rolls-Royce Turbomeca Adour Mk. 951 turbofan with FADEC , 29 kN (6,500 lbf ) 29 kN[source]
Hawk 128 · Up to of weapons on five hardpoints, including
Single sourceUp to 6,800 lb (3,085 kg) of weapons on five hardpoints, including:[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Royal Air Force Indian Air Force Royal Saudi Air Force Royal Australian Air Force South African Air Force[source] | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] |
|---|
| Number built | 1,000+[source] | — |
|---|
| Manufactured | 1974–present[source] | 1985–present[source] |
|---|
| Introduction date | 1976[source] | 1999[source] |
|---|
| First flight | 21 August 1974[source] | November 1985[source] |
|---|
| Developed into | British Aerospace Hawk 200 McDonnell Douglas T-45 Goshawk[source] | — |
|---|
| Useful load | 3,000 kg (6,600 lb)[source] | — |
|---|
| Never exceed speed | Mach 1.2 (in dive)[source] | 341 km/h (212 mph, 184 kn)[source] |
|---|
| Thrust/weight | 0.65[source] | — |
|---|
| Hardpoints | Up to 6,800 lb (3,085 kg) of weapons on five hardpoints, including:[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] |
|---|
| g limits | — | + 6.0/ - 3.0[source] |
|---|
| Country of origin | — | Deutschland[source]Country of design · Entwurfsland |
|---|