NBK 117: Perbedaan antara revisi
Konten dihapus Konten ditambahkan
k Robot: Cosmetic changes |
Tidak ada ringkasan suntingan |
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Baris 35:
== Operator Militer ==
[[File:MBB BK 117-B2 2.jpg|thumb|]]
[[File:LifeStar preparing for takeoff.JPG|thumb|]]
[[File:Hellenic Fire Service BK-117.jpg|thumb|]]
*[[Chili]]
*[[Irak]]
Baris 40 ⟶ 44:
*[[Afrika Selatan]]
*[[United Arab Emirates]]
==Specifications (BK 117-A1)==
{{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
<!-- 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={All the World's Rotorcraft}<ref name="avia-1" />
|crew= Two pilots
|capacity= 10 passengers (varies by model)
|length main= 13 m
|length alt= 35 ft 6 in
|span main= 7 m
|span alt= 36 ft 1 in
|height main= 3.85 m
|height alt= 12 ft 7 in
|area main= <!-- m² -->
|area alt= <!-- ft² -->
|airfoil=
|empty weight main= 1,650 kg
|empty weight alt= 3,630 lb
|loaded weight main= <!-- kg -->
|loaded weight alt= <!-- lb -->
|useful load main= <!-- kg -->
|useful load alt= <!-- kg -->
|max takeoff weight main= 2850 kg
|max takeoff weight alt= 6,270 lb
|more general=
|engine (prop)= [[Honeywell LTS101|Avco Lycoming LTS 101-650B-1]]
[[File:Lts101-750 bht222U aradecki.jpg|thumb|]]
|type of prop= turboshaft
|number of props= 2
|power main= 410 kW
|power alt= 550 shp
|power original=
|max speed main= 262 km/h
|max speed alt= 141 kn, 163 mph
|cruise speed main= 250 km/h
|cruise speed alt= 135 kn, 154 mph
|never exceed speed main= <!-- km/h -->
|never exceed speed alt= <!-- knots, mph -->
|range main= 541 km
|range alt= 292 nmi, 333 mi
|ceiling main= 4,570 m
|ceiling alt = 14,990 ft
|climb rate main= <!-- m/s -->
|climb rate alt= <!-- ft/min -->
|loading main= <!-- kg/m² -->
|loading alt= <!-- lb/ft² -->
|thrust/weight=
|power/mass main= <!-- W/kg -->
|power/mass alt= <!-- hp/lb -->
|more performance=
* '''Hover ceiling:''' 2,530 m (8,300 ft)
|armament=
|avionics=
}}
== Pranala luar ==
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