User:Ericg/experimental/template/test iv

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[edit] Specifications (CH-47 Chinook)

General characteristics

  • Crew: 3
  • Capacity: 44 troops or 24 litters and 2 attendants
  • Length: 68 ft 9 in (30.1 m)
  • Rotor diameter: 60 ft 0 in (18.3 m)
  • Height: 18 ft 8 in (5.7 m)
  • Disc area: 2,830 ft² (263 m²)
  • Empty weight: 22,450 lb (10,185 kg)
  • Loaded weight: lb (kg)
  • Max takeoff weight: 50,000 lb (23,000 kg)
  • Powerplant: 2× Avro Lycoming T55-L-712 turboshafts, 3,750 hp (2,800 kW) each

Performance

Armament

Generated using the text:

== Specifications (CH-47 Chinook) ==
{{Airtemp-test|

|cargo or passengers=yes
|plane or copter=copter
|jet or prop=prop
|military=yes

<!-- Now enter the plane's specifications. -->
|crew=3
|capacity=44 troops or 24 litters and 2 attendants
|length main=68 [[foot (unit of length)|ft]] 9 [[inch|in]]
|length alt=30.1 [[metre|m]]
|span main=60 ft 0 in
|span alt=18.3 m
|height main=18 ft 8 in
|height alt=5.7 m
|area main=2,830 [[square foot|ft²]]
|area alt=263 [[square metre|m²]]
|empty main=22,450 [[pound|lb]]
|empty alt=10,185 [[kilogram|kg]]
|loaded main= lb
|loaded alt= kg
|mtow=50,000 lb
|mtow=23,000 kg
|engine (jet)=
|type of jet=
|number of jets=
|thrust main=
|thrust alt=
|engine (prop)=[[Avro Lycoming T55]]-L-712
|type of prop=[[turboshaft]]s
|number of props=2
|power main=3,750 [[horsepower|hp]]
|power alt=2,800 [[kilowatt|kW]]

|max speed main=159 [[knot (speed)|kt]]
|max speed alt=183 [[miles per hour|mph]], 295 [[kilometre per hour|km/h]]
|cruise speed main= kt
|cruise speed alt= mph,  km/h
|range main=1,110 [[nautical mile|nm]]
|range alt=1,280 [[Mile#Statute miles|mi]], 2,060 [[kilometre|km]]
|ceiling main=8,500 ft
|ceiling alt=2,590 m
|climb rate main=1,980 ft/min
|climb rate alt=10.1 m/s
|performance etc=
|loading main=18 lb/ft²
|loading alt=86 kg/m²
|thrust/weight=
|power/mass main=0.15 hp/lb
|power/mass alt=0.25 kW/kg

|weapons= '''Guns:''' 2× [[M-60]] [[machine gun]]s

}}