Credit
Mztourist · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
combat radius, 4x laser guided bombs, 2x Air-to-air missiles and 1x fuel tank
Single source560 km (350 mi, 300 nmi) (combat radius, 4x laser guided bombs, 2x Air-to-air missiles and 1x fuel tank)[source]
1 × Pratt & Whitney Canada PT6 A-68 turboprop 1,600 shp
Single source1 × Pratt & Whitney Canada PT6 A-68 turboprop , 1,200 kW (1,600 shp)[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]
G 115E · Wing area
Single source12.21 m 2 (131.4 sq ft)[source]
G 115E · 1,050 ft/min
Single source5.3 m/s (1,050 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Calidus B-250 | Grob G 115 |
|---|---|---|
| Type | Military trainer Light attack aircraft[source] | Basic trainer[source] |
| National origin | United Arab Emirates / Brazil[source] | — |
| Manufacturer | Calidus[source] | Grob Aircraft[source] |
| Designer | Novaer[source] | — |
| Status | In production[source] | active[source] |
| Primary user | United Arab Emirates Air Force[source] | — |
| Number built | 2 (as of January 2018)[source] | — |
| First flight | July 2017[source] | November 1985[source] |
| Hardpoints | 7 with a capacity of 1,800 kg (3,960 lb)[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] |
| 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] |
| Country of origin | — | Deutschland[source]Country of design · Entwurfsland |