유로콥터 AS532 쿠거: 두 판 사이의 차이

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→‎제원 (AS532 UB): 번역 안된 틀 제거.
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== 제원 (AS532 UB) ==
[[File:AS332 Super Pum Line Drawing.svg|thumb|right|쿠거의 삼면도]]
 
{{aircraft specifications
 
<!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] -->
 
<!-- please answer the following questions -->
|plane or copter?=copter
|jet or prop?=prop<!-- options: jet/prop/both/neither -->
 
<!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses).
If an item doesn't apply, like capacity, leave it blank. For instructions on using |more general=, |more performance=, |power original=, and |thrust original= see [[Template talk:Aircraft specifications]]. To add a new line, end the old one with a right parenthesis ")" and start a new, fully formatted line beginning with * -->
|ref=Brassey's World Aircraft & Systems Directory<ref name = "brasseys1999">{{cite book |last=Taylor|first=M J H (editor) | title = Brassey's World Aircraft & Systems Directory 1999/2000 Edition | year = 1999 | publisher = Brassey's | isbn = 1 85753 245 7 }}</ref>
|crew=2
|capacity=20 troops
|length main= 15.53 m
|length alt= 50 ft 11½ in
|length more= (fuselage)
|span main= 15.6 m
|span alt= 51 ft 2 in
|height main= 4.92 m
|height alt= 16 ft 2 in
|area main=206 m²
|area alt= 2,217ft²
|airfoil=
|empty weight main= 4,350 kg
|empty weight alt= 9,590 lb
|loaded weight main=
|loaded weight alt=
|useful load main= 4,650 kg
|useful load alt= 10,250 lb
|max takeoff weight main= 9,000 kg
|max takeoff weight alt= 19,840 lb
|more general=
|engine (prop)= [[Turbomeca Makila|Turbomeca Makila 1A1]]
|type of prop= [[turboshaft]]
|number of props=2
|power main= 1,185 kW
|power alt= 1,589 shp
|power original=
|max speed main= 249 km/h
|max speed alt= 134 knots, 154 mph
|cruise speed main= 239 km/h
|cruise speed alt= 129 knots, 148 mph
|stall speed main=
|stall speed alt=
|never exceed speed main= 278 km/h
|never exceed speed alt= 150 knots, 173 mph
|range main= 573 km
|range alt= 310 nm, 357 mi
|ceiling main= 3,450 m
|ceiling alt= 11,319 ft
|climb rate main= 7.2 m/s
|climb rate alt= 1,417 ft/min
|loading main=
|loading alt=
|thrust/weight=
|power/mass main=
|power/mass alt=
|more performance=
|armament=
|avionics=
}}
 
== 같이 보기 ==