FORCETALLY
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At a glance
Measured figures
DART-450, utility (reconnaissance · Length
Single source10.75 m (35 ft 3 in)[source]
Configuration
| Specification | Diamond DART series | Grob G 115 |
|---|---|---|
| Type | Two-seat military training aircraft[source] | Basic trainer[source] |
| National origin | Austria[source] | — |
| Manufacturer | Diamond Aircraft[source] | Grob Aircraft[source] |
| First flight | 17 May 2016 (DART 450)[source] | November 1985[source] |
G 115E · Length
7.79 m (25 ft 7 in)[source]
Empty; DART-450, utility (reconnaissance · Empty weight
Single sourceMaximum take-off; DART-450, utility (reconnaissance · Max takeoff weight
Single source1,330 kg (2,932 lb)[source]
2,300 kg (5,071 lb)[source]
Empty; G 115E · Empty weight
Single sourceMaximum take-off; G 115E · Max takeoff weight
Single sourceCruise; DART-450, utility (reconnaissance · Cruise speed
Single sourceMaximum; DART-450, utility (reconnaissance · Maximum speed
Single source460 km/h (290 mph, 250 kn)[source]
430 km/h (260 mph, 230 kn)[source]
Cruise; G 115E · long range cruising speed
Single sourceMaximum; G 115E · Maximum speed
Single sourceDART-450, utility (reconnaissance · 1 × Ivchenko-Progress Motor Sich AI-450S turboprop
Single source1 × Ivchenko-Progress Motor Sich AI-450S turboprop, 369 kW (495 hp)[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]
DART-450, utility (reconnaissance · Endurance
Single source8 hr 10 min[source]
G 115E · Wing area
Single source12.21 m 2 (131.4 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Developed into | UZGA UTS-800[source] | — |
|---|
| Fuel capacity | 850 L (190 imp gal; 220 US gal) usable[source] | 143 L (31 imp gal; 38 US gal) usable[source] |
|---|
| Propellers | 5-bladed MT Propeller[source] | 3-bladed Hoffmann HO-V343K-V/183GY Constant-speed propeller , 1.83 m (6 ft 0 in) diameter[source] |
|---|
| Stall speed | 110 km/h (69 mph, 60 kn)[source] | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] |
|---|
| g limits | +7/-4G[source] | + 6.0/ - 3.0[source] |
|---|
| Take-off run | 600 m (2,000 ft)[source] | — |
|---|
| Landing run | 400 m (1,300 ft)[source] | — |
|---|
| fuel burn | 90 litres/hour[source] | — |
|---|
| operating cost | $500/hour[source] | — |
|---|
| Status | — | active[source] |
|---|
| Primary users | — | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] |
|---|
| Manufactured | — | 1985–present[source] |
|---|
| Introduction date | — | 1999[source] |
|---|
| Aspect ratio | — | 8.2:1[source] |
|---|
| Airfoil | — | Eppler 696[source] |
|---|
| Never exceed speed | — | 341 km/h (212 mph, 184 kn)[source] |
|---|
| Country of origin | — | Deutschland[source]Country of design · Entwurfsland |
|---|
| Reported operators |
| — |
|---|