User:Ingoolemo/Airspec demo

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Contents 1 Specifications (Boeing 787-3) 2 Specifications (Convair B-36J) 3 Specifications (CH-47 Chinook) 4 Specifications (Wikimedia Wikiglider-3)

[edit] Specifications (Boeing 787-3)

General characteristics

• Crew: 3?
• Capacity: 269 passengers
• Length: 182 ft 1 in (55.5 m)
• Wingspan: 169 ft 4 in (51.6 m)
• Height: 54 ft 2 in (16.5 m)
• Wing area: ft² (m²)
• Empty weight: 289,900 lb (131,500 kg)
• Loaded weight: lb (kg)
• Max takeoff weight: 360,400 lb (163,500 kg)
• Powerplant: 2× General Electric GEnx turbofans, 75,000 lbf (334 kN) each

Performance

• Maximum speed: kt (mph, km/h)
• Cruise speed: 560 kt (650 mph, 1,000 km/h)
• Range: 3,500 nm (4,000 mi, 6,500 km)
• Service ceiling: 43,000 ft (13,000 m)
• Rate of climb: ft/min (m/s)
• Wing loading: lb/ft² (kg/m²)
• Thrust/weight: 0.42

Generated using the text:

== Specifications (Boeing 787-3) ==
{{aircraft specifications|

|include 'capacity' field?=yes
|plane or copter?=plane
|jet or prop?=jet
|include 'armament' field?=no
|switch order of units?=no

|crew=3?
|capacity=269 passengers
|length main=182 [[foot (unit of length)|ft]] 1 [[inch|in]]
|length alt=55.5 [[metre|m]]
|span main=169 ft 4 in
|span alt=51.6 m
|height main=54 ft 2 in
|height alt=16.5 m
|area main= [[square foot|ft²]]
|area alt= [[square metre|m²]]
|empty weight main=289,900 [[pound (mass)|lb]]
|empty weight alt=131,500 [[kilogram|kg]]
|loaded weight main= lb
|loaded weight alt= kg
|max takeoff weight main=360,400 lb
|max takeoff weight alt=163,500 kg
|engine (jet)=[[General Electric GEnx]]
|type of jet= [[turbofan]]s
|number of jets=2
|thrust main=75,000 [[pound-force|lbf]]
|thrust alt=334 [[kilonewton|kN]]
|engine (prop)=
|type of prop=
|number of props=
|power main=
|power alt=

|max speed main= [[knot (speed)|kt]]
|max speed alt= [[miles per hour|mph]],  [[kilometre per hour|km/h]]
|cruise speed main=560 kt
|cruise speed alt=650 mph, 1,000 km/h
|range main=3,500 [[nautical mile|nm]]
|range alt=4,000 [[statute mile|mi]], 6,500 [[kilometre|km]]
|ceiling main=43,000 ft
|ceiling alt=13,000 m
|climb rate main= ft/min
|climb rate alt= m/s
|loading main= lb/ft²
|loading alt= kg/m²
|thrust/weight=0.42
|power/mass main=
|power/mass alt=

|armament=

}}

[edit] Specifications (Convair B-36J)

General characteristics

• Crew: 15
• Length: 162 ft 1 in (49.40 m)
• Wingspan: 230 ft 0 in (70.10 m)
• Height: 46 ft 8 in (14.22 m)
• Wing area: 4,772 ft² (443 m²)
• Empty weight: 171,035 lb (77,580 kg)
• Loaded weight: lb (kg)
• Max takeoff weight: 410,000 lb (190,000 kg)
• Powerplant:
  • 4× General Electric J47 turbojets, 5,200 lbf (23 kN) each
  • 6× Pratt & Whitney R-4360-51 'Wasp Major' radials, 3,800 hp (2,500 kW) each

Performance

• Maximum speed: 380 kt (439 mph, 707 km/h)
• Cruise speed: kt (mph, km/h)
• Range: 7,000 nm (8,000 mi, 13,000 km)
• Service ceiling: 48,000 ft (15,000 m)
• Rate of climb: 1,920 ft/min (9.75 m/s)
• Wing loading: 55.76 lb/ft² (272.3 kg/m²)
• Power/mass (prop): 0.086 hp/lb (0.12 kW/kg)
• Thrust/weight (jet): 0.078

Armament

• Guns: 16× M24-A1 cannon
• Bombs: 86,000 lb (39,000 kg)

Generated using the text:

== Specifications (Convair B-36J) ==
{{aircraft specifications|

|include 'capacity' field?=no
|plane or copter?=plane
|jet or prop?=both
|include 'armament' field?=yes
|switch order of units?=no

|crew=15
|capacity=
|length main=162 [[foot (unit of length)|ft]] 1 [[inch|in]]
|length alt=49.40 [[metre|m]]
|span main=230 ft 0 in
|span alt=70.10 m
|height main=46 ft 8 in
|height alt=14.22 m
|area main=4,772 [[square foot|ft²]]
|area alt=443 [[square metre|m²]]
|empty weight main=171,035 [[pound (mass)|lb]]
|empty weight alt=77,580 [[kilogram|kg]]
|loaded weight main= lb
|loaded weight alt= kg
|max takeoff weight main=410,000 lb
|max takeoff weight alt=190,000 kg
|engine (prop)=[[Pratt & Whitney R-4360]]-51
|type of prop= 'Wasp Major' radials
|number of props=6
|power main=3,800 [[horsepower|hp]]
|power alt=2,500 [[kilowatt|kW]]
|engine (jet)=[[General Electric J47]]
|type of jet= [[turbojet]]s
|number of jets=4
|thrust main=5,200 [[pound-force|lbf]]
|thrust alt=23 [[kilonewton|kN]]

|max speed main=380 [[knot (speed)|kt]]
|max speed alt=439 [[miles per hour|mph]], 707 [[kilometre per hour|km/h]]
|cruise speed main= kt
|cruise speed alt= mph,  km/h
|range main=7,000 [[nautical mile|nm]]
|range alt=8,000 [[statute mile|mi]], 13,000 [[kilometre|km]]
|ceiling main=48,000 ft
|ceiling alt=15,000 m
|climb rate main=1,920 ft/min
|climb rate alt=9.75 m/s
|loading main=55.76 lb/ft²
|loading alt=272.3 kg/m²
|thrust/weight=0.078
|power/mass main=0.086 hp/lb
|power/mass alt=0.12 kW/kg

|armament=
* '''Guns:''' 16× [[M24]]-A1 [[autocannon|cannon]]
* '''Bombs:''' 86,000 lb (39,000 kg)

}}

[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

• Maximum speed: 159 kt (183 mph, 295 km/h)
• Cruise speed: kt (mph, km/h)
• Range: 1,110 nm (1,280 mi, 2,060 km)
• Service ceiling: 8,500 ft (2,590 m)
• Rate of climb: 1,980 ft/min (10.1 m/s)
• Disc loading: 18 lb/ft² (86 kg/m²)
• Power/mass: 0.15 hp/lb (0.25 kW/kg)

Armament

• Guns: 2× M-60 machine guns

Generated using the text:

== Specifications (CH-47 Chinook) ==
{{aircraft specifications|

|include 'capacity' field?=yes
|plane or copter?=copter
|jet or prop?=prop
|include 'armament' field?=yes
|switch order of units?=no

<!-- 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 weight main=22,450 [[pound (mass)|lb]]
|empty weight alt=10,185 [[kilogram|kg]]
|loaded weight main= lb
|loaded weight alt= kg
|max takeoff weight main=50,000 lb
|max takeoff weight alt=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 [[statute mile|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
|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

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

}}

[edit] Specifications (Wikimedia Wikiglider-3)

General characteristics

• Crew: 1
• Capacity: 1 passenger
• Length: 6.12 m (20 ft 1 in)
• Wingspan: 169 ft 4 in (51.6 m)
• Height: 2.4 m (8 ft 0 in)
• Wing area: 15.8 m² (170 ft²)
• Empty weight: 40 kg (80 lb)
• Loaded weight: 160 kg (320 lb)
• Max takeoff weight: 163,500 kg (360,400 lb)

Performance

• Maximum speed: 1,300 km/h (700 kt, 810 mph)
• Cruise speed: 1,000 km/h (560 kt, 650 mph)
• Range: 6,500 km (3,500 nm, 4,000 mi)
• Service ceiling: 13,000 m (43,000 ft)
• Rate of climb: 1 m/s (200 ft/min)
• Wing loading: 10 kg/m² (1.9 lb/ft²)

Generated using the text:

== Specifications (Wikimedia Wikiglider-3) ==
{{User:Ingoolemo/Airspec|

|include 'capacity' field?=yes
|plane or copter?=plane
|jet or prop?=neither
|has armament?=no
|has avionics?=no

|crew=1
|capacity=1 passenger
|length main=6.12 [[metre|m]]
|length alt=20 [[foot (unit of length)|ft]] 1 [[inch|in]]
|span main=169 ft 4 in
|span alt=51.6 m
|height main=2.4 m
|height alt=8 ft 0 in
|area main=15.8 [[square metre|m²]]
|area alt=170 [[square foot|ft²]]
|empty weight main=40 [[kilogram|kg]]
|empty weight alt=80 [[pound (mass)|lb]]
|loaded weight main=160 kg
|loaded weight alt=320 lb
|maximum takeoff weight main=163,500 kg
|maximum takeoff weight alt=360,400 lb
|engine (jet)=
|type of jet=
|number of jets=
|thrust main=
|thrust alt=
|engine (prop)=
|type of prop=
|number of props=
|power main=
|power alt=

|max speed main=1,300 [[kilometre per hour|km/h]]
|max speed alt=700 [[knot (speed)|kt]], 810 [[miles per hour|mph]]
|cruise speed main=1,000 km/h
|cruise speed alt=560 kt, 650 mph
|range main=6,500 [[kilometre|km]]
|range alt=3,500 [[nautical mile|nm]], 4,000 [[statute mile|mi]]
|ceiling main=13,000 m
|ceiling alt=43,000 ft
|climb rate main=1 m/s
|climb rate alt=200 ft/min
|loading main=10 kg/m²
|loading alt=1.9 lb/ft²
|thrust/weight=
|power/mass main=
|power/mass alt=

|armament=

}}