CASA CN 235: Revizyonlar arasındaki fark
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İçerik silindi İçerik eklendi
k r2.7.3) (Bot: Değiştiriliyor: fr:Airtech CN-235 |
Değişiklik özeti yok |
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68. satır:
* {{UAE}}:12
==Teknik Özellikler==
[[File:EADS CASA CN-235.svg|250px|right]]
{{aircraft specifications
|plane or copter?=plane
|jet or prop?=prop
|crew=2
|capacity=44 passengers
|payload main=5,950 kg<ref>[http://www.airbusmilitary.com/Tactical/TactCN235.aspx Specifications - Performance - CN235]</ref>
|payload alt=13,120 lb
|payload more=
|length main= 21.40 m
|length alt= 70 ft 2½ in
|span main= 25.81 m
|span alt= 84 ft 8 in
|height main= 8.18 m
|height alt= 26 ft 10 in
|area main= 59.10 m²
|area alt= 636.1 sq st
|airfoil=NACA 65<sub>3</sub>-218
|aspect ratio=11.27:1
|empty weight main= 9,800 kg
|empty weight alt= 21,605 lb
|loaded weight main=
|loaded weight alt=
|useful load main= 48.54 m3
|useful load alt= 1715.17 ft3
|max takeoff weight main= 16,500 kg
|max takeoff weight alt= 36,380 lb
|more general=
|engine (prop)= [[General Electric T700|General Electric CT7]]-9C3
|type of prop=[[turboprop]]s
|number of props=2
|power main= 1,750 shp
|power alt=
|power original=
|max speed main=
|max speed alt=
|cruise speed main=454 km/h
|cruise speed alt=245 knots,
|stall speed main=
|stall speed alt=
|never exceed speed main=
|never exceed speed alt=
|range main= 5,055 km
|range alt=2730 nm
|range more=
|ceiling main= 7,620 m
|ceiling alt= 25,000 ft
|climb rate main= 7.8 m/s
|climb rate alt= 1,780 ft/min
|loading main=
|loading alt=
|thrust/weight=
|power/mass main=
|power/mass alt=
|more performance=
|armament=
|avionics=
}}
<gallery>
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