CL-28 / CP-107 Argus
MODEL | CL-28 "Argus" Mk.I | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
VARIANTS |
CREW | 15 / 5 + 6 operators | ENGINE | 4 x Wright R-3350-EA1 Turbo-Compound Cyclone | Power | 2535kW | 4 x 3400 hp | WEIGHTS | Maximum Take-off weight | 71,214 kg | 157,000 lb | normal take-off | 67,133kg | lb | Empty weight | 36,741 kg | 81000 lb | Internal fuel | 32,776 liters | gal | DIMENSIONS | Wingspan | 43.37 m | 142 ft 3 in | Length | 39.26 m | 129 ft 10 in | Height | 11.79 m | 39 ft 8 in | Wing area | 192.77 m2 | 2074.96 sq ft | PERFORMANCE | Max. speed | 507 km/h | 315 mph | Cruising speed | 463 km/h | | Ceiling | 7,620 m | 25,000 ft | Range | 9,495 km | 5,900 miles | Range of action | 6437 km | miles | Flight duration | 26.30 h. Min
| ARMAMENT |
5352 kg in 2 weapons bays and 2 hard points
| 3,629kg of weapons inside the fuselage 1,724kg on external hardpoints |
NEWSLETTER
|
Join the GlobalSecurity.org mailing list |
|
|