Difference between revisions of "Template:Aircraft specifications"

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<noinclude>{{esoteric}}[[Category:Templates using ParserFunctions|{{PAGENAME}}]]
+
<noinclude>{{Being deleted|2019 March 20|Template:Aerospecs|merge=Template:Aircraft specs}}</noinclude><noinclude>{{Deprecated|Aircraft specifications|Aircraft specs|date=March 2019}}</noinclude>
'''Editors beware:''' formatting of code to make it "look nice" is very likely to inadvertently introduce leading and trailing blank lines into the template output.
+
{{
</noinclude>{{
+
#if: {{{ref|}}}
#if:{{{ref|}}}
+
  |<p style="font-size: 90%; margin:0; padding: .2em">''Data from'' {{{ref}}}</p>
  |<p style="font-size: 90%; margin:0;">''Data from'' {{{ref}}}</p>
+
}}<span style="font-size: 120%;">'''General characteristics'''</span>{{
}}<h3 style="padding-top: .2em;">General characteristics<h3>{{
+
#if: {{{crew|}}}
#if:{{{crew|}}}
+
  |* '''Crew:''' {{{crew}}}
  |* '''Crew:''' {{{crew|}}}
 
 
}}{{
 
}}{{
#if:{{{capacity|}}}
+
#if: {{{capacity|}}}
 
  |* '''Capacity:''' {{{capacity}}}
 
  |* '''Capacity:''' {{{capacity}}}
 
}}{{
 
}}{{
#if:{{{payload main|}}}
+
#if: {{{payload main|}}}
  |* '''[[Payload]]:''' {{{payload main|}}} ({{{payload alt|}}}) {{{payload more|}}}
+
  |* '''[[Payload]]:''' {{{payload main}}} ({{{payload alt|}}}) {{{payload more|}}}
}}
 
* '''Length:''' {{{length main|}}} ({{{length alt|}}}){{
 
#ifeq:{{{plane or copter?}}}|copter
 
|* '''Rotor diameter:''' {{{span main|}}} ({{{span alt|}}})
 
|* '''[[Wingspan]]:''' {{{span main|}}} ({{{span alt|}}})
 
 
}}
 
}}
 +
* '''Length:''' {{{length main|}}} ({{{length alt|}}})
 +
* '''{{#ifeq: {{{plane or copter?}}} | copter
 +
|Rotor diameter
 +
|[[Wingspan]]
 +
}}:''' {{{span main|}}} ({{{span alt|}}})
 
* '''Height:''' {{{height main|}}} ({{{height alt|}}}){{
 
* '''Height:''' {{{height main|}}} ({{{height alt|}}}){{
 
#if:{{{area main|}}}
 
#if:{{{area main|}}}
  |{{
+
  |* '''{{
  #ifeq:{{{plane or copter?}}}|copter
+
  #ifeq: {{{plane or copter?}}} | copter
   |* '''Disc area:''' {{{area main|}}} ({{{area alt|}}})
+
   |Disc
   |* '''Wing area:''' {{{area main|}}} ({{{area alt|}}})
+
   |Wing
}}
+
}} area:''' {{{area main}}} ({{{area alt|}}})
 
}}{{
 
}}{{
#if:{{{airfoil|}}}
+
#if: {{{airfoil|}}}
 
  |* '''[[Airfoil]]:''' {{{airfoil}}}
 
  |* '''[[Airfoil]]:''' {{{airfoil}}}
 
}}{{
 
}}{{
#if:{{{empty weight main|}}}
+
#if: {{{aspect ratio|}}}
  |* '''Empty weight:''' {{{empty weight main|}}} ({{{empty weight alt|}}})
+
  |* '''[[Aspect ratio (aeronautics)|Aspect ratio]]:''' {{{aspect ratio}}}
 
}}{{
 
}}{{
#if:{{{loaded weight main|}}}
+
#if: {{{empty weight main|}}}
  |* '''Loaded weight:''' {{{loaded weight main|}}} ({{{loaded weight alt|}}})
+
  |* '''[[Manufacturer's empty weight|Empty weight]]:''' {{{empty weight main|}}} ({{{empty weight alt|}}})
 
}}{{
 
}}{{
#if:{{{useful load main|}}}
+
#if: {{{useful load main|}}}
 
  |* '''Useful load:''' {{{useful load main|}}} ({{{useful load alt|}}})
 
  |* '''Useful load:''' {{{useful load main|}}} ({{{useful load alt|}}})
 
}}{{
 
}}{{
#if:{{{max takeoff weight main|}}}
+
#if: {{{loaded weight main|}}}
  |* '''[[Maximum Take-Off Weight|Max takeoff weight]]:''' {{{max takeoff weight main|}}} ({{{max takeoff weight alt|}}}) {{{max takeoff weight more|}}}
+
  |* '''Loaded weight:''' {{{loaded weight main|}}} ({{{loaded weight alt|}}}) {{{loaded weight more|}}}
 
}}{{
 
}}{{
#switch:{{{jet or prop?|}}}
+
#if: {{{max takeoff weight main|}}}
  |prop=* '''Powerplant:''' {{{number of props|}}}× {{{engine (prop)|}}} {{{type of prop|}}}, {{{power main|}}} ({{{power alt|}}}){{{power original|}}} {{{power more|}}} {{
+
|* '''[[Maximum takeoff weight|Max. takeoff weight]]:''' {{{max takeoff weight main}}} ({{{max takeoff weight alt|}}}) {{{max takeoff weight more|}}}
  #ifeq:{{{number of props}}}|1
+
}}{{
  |
+
#if: {{{more general|}}}
 +
  |* {{{more general}}}
 +
}}{{
 +
#switch: {{{jet or prop?}}}
 +
  |prop =* '''[[Aircraft engine|Powerplant]]:''' {{{number of props|}}} × {{{engine (prop)|}}}{{#if: {{{type of prop|}}} |&#32;{{{type of prop}}} }}, {{{power main|}}} ({{{power alt|}}}){{{power original|}}} {{{power more|}}} {{
 +
  #ifeq: {{{number of props}}} |1 |
 
   |each
 
   |each
 
  }}{{
 
  }}{{
  #if:{{{propellers|}}}
+
  #if: {{{propellers|}}}
   |* '''Propellers:''' {{{propellers|}}} {{{propeller or rotor?|}}}{{
+
   |* '''Propellers:''' {{{propellers}}} {{{propeller or rotor?|}}}{{
   #if:{{{number of propellers per engine|}}}
+
   #if: {{{number of propellers per engine|}}}
   |, {{{number of propellers per engine|}}} per engine
+
   |, {{{number of propellers per engine}}} per engine
  }}{{
 
  #if:{{{propeller diameter main|}}}
 
  |** '''Propeller diameter:''' {{{propeller diameter main|}}} ({{{propeller diameter alt|}}})
 
 
   }}
 
   }}
 
  }}{{
 
  }}{{
 
  #if:{{{propeller diameter main|}}}
 
  #if:{{{propeller diameter main|}}}
   |{{
+
   |{{ #if: {{{propellers|}}} |**|*}} '''Propeller diameter:''' {{{propeller diameter main}}} ({{{propeller diameter alt|}}})
  #if:{{{propellers|}}}
 
  |
 
  |* '''Propeller diameter:''' {{{propeller diameter main|}}} ({{{propeller diameter alt|}}})
 
  }}
 
 
  }}
 
  }}
  |jet=* '''Powerplant:''' {{{number of jets|}}}× {{{engine (jet)|}}} {{{type of jet|}}}{{
+
  | jet =* '''[[Aircraft engine|Powerplant]]:''' {{{number of jets|}}} × {{{engine (jet)|}}} {{{type of jet|}}}{{
   #if:{{{thrust main|}}}
+
   #if: {{{thrust main|}}}
|{{
+
  |{{
#if:{{{afterburning thrust main|}}}
+
    #if: {{{afterburning thrust main|}}}
  |** '''Dry thrust:''' {{{thrust main|}}} ({{{thrust alt|}}}){{{thrust original|}}} {{
+
    |** '''Dry thrust:''' {{{thrust main}}} ({{{thrust alt|}}}) {{{thrust original|}}} {{
  #ifeq:{{{number of jets}}}|1
+
    #ifeq: {{{number of jets}}} |1
    |
+
      |
    |each
+
      |each
  }}
+
    }}
** '''Thrust with [[afterburner]]:''' {{{afterburning thrust main|}}} ({{{afterburning thrust alt|}}}){{{afterburning thrust original|}}} {{
+
** '''Thrust with [[afterburner]]:''' {{{afterburning thrust main}}} ({{{afterburning thrust alt|}}}) {{{afterburning thrust original|}}} <!--
  #ifeq:{{{number of jets}}}|1
+
 
     |
+
     follows ELSE branch of if [NOT] afterburning
    |each
+
 
  }}
+
  -->
  |, {{{thrust main|}}} ({{{thrust alt|}}}){{{thrust original|}}} {{{thrust more|}}} {{
+
    |, {{{thrust main}}} ({{{thrust alt|}}}){{{thrust original|}}} {{{thrust more|}}}
   #ifeq:{{{number of jets}}}|1
+
    }}<!--endif afterburning thrust; now show # of jets whether for afterburner or main --> {{
    |
+
   #ifeq: {{{number of jets}}} | 1 |
     |each
+
     |each }}
  }}
 
  }}
 
 
  }}
 
  }}
  |both=* '''Powerplant:'''
+
  |both=* '''[[Aircraft engine|Powerplant]]:'''
** {{{number of jets|}}}× {{{engine (jet)|}}} {{{type of jet|}}}, {{{thrust main|}}} ({{{thrust alt|}}}){{{thrust original|}}} {{{thrust more|}}} {{
+
** {{{number of jets|}}} × {{{engine (jet)|}}}{{#if: {{{type of jet|}}} |&#32;{{{type of jet}}} }}, {{{thrust main|}}} ({{{thrust alt|}}}){{{thrust original|}}} {{{thrust more|}}} {{
 
  #ifeq:{{{number of jets}}}|1
 
  #ifeq:{{{number of jets}}}|1
 
   |
 
   |
 
   |each
 
   |each
 
  }}
 
  }}
** {{{number of props|}}}× {{{engine (prop)|}}} {{{type of prop|}}}, {{{power main|}}} ({{{power alt|}}}){{{power original|}}} {{{power more|}}} {{
+
** {{{number of props|}}} × {{{engine (prop)|}}}{{#if: {{{type of prop|}}} |&#32;{{{type of prop}}} }}, {{{power main|}}} ({{{power alt|}}}) {{{power original|}}} {{{power more|}}} {{
 
  #ifeq:{{{number of props}}}|1
 
  #ifeq:{{{number of props}}}|1
 
   |
 
   |
 
   |each
 
   |each
 
  }}{{
 
  }}{{
  #if:{{{propellers|}}}
+
  #if: {{{propellers|}}}
   |*** '''Propellers:''' {{{propellers|}}} {{{propeller or rotor?|}}}{{
+
   |*** '''Propellers:''' {{{propellers}}} {{{propeller or rotor?|}}}{{
 
   #if:{{{number of propellers per engine|}}}
 
   #if:{{{number of propellers per engine|}}}
   |, {{{number of propellers per engine|}}} per engine
+
   |, {{{number of propellers per engine}}} per engine
 
   }}{{
 
   }}{{
   #if:{{{propeller diameter main|}}}
+
   #if: {{{propeller diameter main|}}}
   |** '''Propeller diameter:''' {{{propeller diameter main|}}} ({{{propeller diameter alt|}}})
+
   |** '''Propeller diameter:''' {{{propeller diameter main}}} ({{{propeller diameter alt|}}})
 
   }}
 
   }}
 
  }}{{
 
  }}{{
 
  #if:{{{propeller diameter main|}}}
 
  #if:{{{propeller diameter main|}}}
 
   |{{
 
   |{{
   #if:{{{propellers|}}}
+
   #if: {{{propellers|}}}
 
   |
 
   |
   |* '''Propeller diameter:''' {{{propeller diameter main|}}} ({{{propeller diameter alt|}}})
+
   |* '''Propeller diameter:''' {{{propeller diameter main}}} ({{{propeller diameter alt|}}})
 
   }}
 
   }}
 
  }}
 
  }}
 
}}{{
 
}}{{
  #if:{{{more general|}}}
+
  #if: {{{more general powerplant|}}}
   |* {{{more general|}}}
+
   |{{{more general powerplant}}}
 
}}
 
}}
<h3>{{{performance header|Performance}}}<h3>
+
<span style="font-size: 120%;">{{{performance header|'''Performance'''}}}</span>
 
{{
 
{{
#if:{{{never exceed speed main|}}}
 
|* '''[[Vne|Never exceed speed]]:''' {{{never exceed speed main|}}} {{#if:{{{never exceed speed alt|}}}
 
  |({{{never exceed speed alt|}}}) {{{never exceed speed more|}}}
 
}}
 
}}{{
 
 
#if:{{{max speed main|}}}
 
#if:{{{max speed main|}}}
  |* '''[[Vno|Maximum speed]]:''' {{{max speed main|}}} {{
+
  |* '''[[V speeds#Regulatory_V-speeds|Maximum speed]]:''' {{{max speed main}}} {{
 
  #if:{{{max speed alt|}}}
 
  #if:{{{max speed alt|}}}
   |({{{max speed alt|}}}) {{{max speed more|}}}
+
   |({{{max speed alt}}}) {{{max speed more|}}}
 
  }}
 
  }}
 
}}{{
 
}}{{
 
#if:{{{cruise speed main|}}}
 
#if:{{{cruise speed main|}}}
  |* '''[[VC speed|Cruise speed]]:''' {{{cruise speed main|}}} {{
+
  |* '''[[V speeds#Vc|Cruise speed]]:''' {{{cruise speed main|}}} {{
 
  #if:{{{cruise speed alt|}}}
 
  #if:{{{cruise speed alt|}}}
 
   |({{{cruise speed alt|}}}) {{{cruise speed more|}}}
 
   |({{{cruise speed alt|}}}) {{{cruise speed more|}}}
 
  }}
 
  }}
 
}}{{
 
}}{{
#if:{{{stall speed main|}}}
+
#if: {{{stall speed main|}}}
  |* '''[[Stall speed]]:''' {{{stall speed main|}}} ({{{stall speed alt|}}}) {{{stall speed more|}}}
+
  |* '''[[Stall speed]]:''' {{{stall speed main}}} ({{{stall speed alt|}}}) {{{stall speed more|}}}
 +
}}{{
 +
#if: {{{never exceed speed main|}}}
 +
|* '''[[V speeds#Vne|Never exceed speed]]:''' {{{never exceed speed main}}} {{#if:{{{never exceed speed alt|}}}
 +
  |({{{never exceed speed alt}}}) {{{never exceed speed more|}}}
 +
}}
 
}}{{
 
}}{{
#if:{{{minimum control speed main|}}}
+
#if: {{{minimum control speed main|}}}
  |* '''[[Vmc|Minimum controllable speed]]:''' {{{minimum control speed main|}}} ({{{minimum control speed alt|}}}) {{{minimum control speed more|}}}
+
  |* '''[[V speeds#Vmc|Minimum controllable speed]]:''' {{{minimum control speed main}}} ({{{minimum control speed alt|}}}) {{{minimum control speed more|}}}
 
}}{{
 
}}{{
 
#if:{{{range main|}}}
 
#if:{{{range main|}}}
  |* '''[[Range (aircraft)|Range]]:''' {{{range main|}}} ({{{range alt|}}}) {{{range more|}}}
+
  |* '''[[Range (aeronautics)|Range]]:''' {{{range main}}} ({{{range alt|}}}) {{{range more|}}}
 
}}{{
 
}}{{
 
#if:{{{combat radius main|}}}
 
#if:{{{combat radius main|}}}
  |* '''Combat radius:''' {{{combat radius main|}}} ({{{combat radius alt|}}}) {{{combat radius more|}}}
+
  |* '''[[Combat radius]]:''' {{{combat radius main}}} ({{{combat radius alt|}}}) {{{combat radius more|}}}
 
}}{{
 
}}{{
 
#if:{{{combat range main|}}}
 
#if:{{{combat range main|}}}
  |*'''Combat range:''' {{{combat range main|}}} ({{{combat range alt|}}}) {{{combat range more|}}}
+
  |*'''Combat range:''' {{{combat range main}}} ({{{combat range alt|}}}) {{{combat range more|}}}
 
}}{{
 
}}{{
 
#if:{{{ferry range main|}}}
 
#if:{{{ferry range main|}}}
  |* '''Ferry range:''' {{{ferry range main|}}} ({{{ferry range alt|}}}) {{{ferry range more|}}}
+
  |* '''[[Range (aeronautics)|Ferry range]]:''' {{{ferry range main}}} ({{{ferry range alt|}}}) {{{ferry range more|}}}
 +
}}{{
 +
#if: {{{endurance|}}}
 +
|* '''[[Endurance (aeronautics)|Endurance]]:''' {{{endurance}}}
 +
}}{{
 +
#if: {{{ceiling main|}}}
 +
|* '''[[Ceiling (aeronautics)|Service ceiling]]:''' {{{ceiling main}}} ({{{ceiling alt|}}}) {{{ceiling more|}}}
 
}}{{
 
}}{{
#if:{{{ceiling main|}}}
+
#if: {{{climb rate main|}}}
  |* '''[[Service ceiling]]:''' {{{ceiling main|}}} ({{{ceiling alt|}}}) {{{ceiling more|}}}
+
  |* '''[[Rate of climb]]:''' {{{climb rate main}}} ({{{climb rate alt|}}}) {{{climb rate more|}}}
 
}}{{
 
}}{{
#if:{{{climb rate main|}}}
+
#if: {{{sink rate main|}}}
  |* '''[[Rate of climb]]:''' {{{climb rate main|}}} ({{{climb rate alt|}}}) {{{climb rate more|}}}
+
  |* '''[[Rate of climb|sink rate]]:''' {{{sink rate main}}} ({{{sink rate alt|}}}) {{{sink rate more|}}}
 
}}{{
 
}}{{
#ifeq:{{{plane or copter?}}}|copter
+
#if: {{{glide ratio|}}}
  |{{
+
  |* '''[[Gliding flight#Glide ratio|Glide ratio]]:''' {{{glide ratio}}}
#if:{{{loading main|}}}
+
}}{{
  |* '''Disc loading:''' {{{loading main|}}} ({{{loading alt|}}})
+
#if: {{{loading main|}}}
}}
+
|* '''{{#ifeq: {{{plane or copter?}}} |copter
|{{
+
          |[[Disk loading|Disc loading]]
#if:{{{loading main|}}}
+
          |[[Wing loading]]
  |* '''[[Wing loading]]:''' {{{loading main|}}} ({{{loading alt|}}})
+
        }}:''' {{{loading main}}} ({{{loading alt|}}})
  }}
+
}}{{
 +
#if:{{{lift to drag|}}}
 +
|* '''[[Lift-to-drag ratio|lift-to-drag]]:''' {{{lift to drag}}}
 +
}}{{
 +
#if:{{{fuel consumption|}}}
 +
  |* '''[[Fuel efficiency|Fuel consumption]]:''' {{{fuel consumption}}}
 
}}{{
 
}}{{
#switch:{{{jet or prop?}}}
+
#switch: {{{jet or prop?}}}
  |jet={{#if:{{{afterburning thrust/weight|}}}
+
  |jet={{ #if: {{{afterburning thrust/weight|}}}
 
   |* '''[[Thrust-to-weight ratio|Thrust/weight]]:'''{{
 
   |* '''[[Thrust-to-weight ratio|Thrust/weight]]:'''{{
 
   #if:{{{thrust/weight|}}}
 
   #if:{{{thrust/weight|}}}
   |** '''Dry:''' {{{thrust/weight|}}}
+
   |** '''Dry:''' {{{thrust/weight}}}
 
   }}
 
   }}
** '''With afterburner:''' {{{afterburning thrust/weight|}}}
+
** '''With afterburner:''' {{{afterburning thrust/weight}}}
 
   |{{
 
   |{{
 
   #if:{{{thrust/weight|}}}
 
   #if:{{{thrust/weight|}}}
   |* '''[[Thrust-to-weight ratio|Thrust/weight]]:''' {{{thrust/weight|}}}
+
   |* '''[[Thrust-to-weight ratio|Thrust/weight]]:''' {{{thrust/weight}}}
 
   }}
 
   }}
 
  }}
 
  }}
 
  |prop={{
 
  |prop={{
 
  #if:{{{power/mass main|}}}
 
  #if:{{{power/mass main|}}}
   |* '''[[Power-to-weight ratio|Power/mass]]:''' {{{power/mass main|}}} ({{{power/mass alt|}}})
+
   |* '''[[Power-to-weight ratio|Power/mass]]:''' {{{power/mass main}}} ({{{power/mass alt|}}})
 
  }}
 
  }}
 
  |both={{
 
  |both={{
 
  #if:{{{power/mass main|}}}
 
  #if:{{{power/mass main|}}}
   |* '''[[Power-to-weight ratio|Power/mass]] (prop):''' {{{power/mass main|}}} ({{{power/mass alt|}}})
+
   |* '''[[Power-to-weight ratio|Power/mass]] (prop):''' {{{power/mass main}}} ({{{power/mass alt|}}})
 
  }}{{
 
  }}{{
 
  #if:{{{thrust/weight|}}}
 
  #if:{{{thrust/weight|}}}
   |* '''[[Thrust-to-weight ratio|Thrust/weight]] (jet):''' {{{thrust/weight|}}}
+
   |* '''[[Thrust-to-weight ratio|Thrust/weight]] (jet):''' {{{thrust/weight}}}
 
  }}
 
  }}
|
 
 
}}{{
 
}}{{
#ifeq:{{{plane or copter?}}}|copter
+
#if: {{{max loading main|}}}
|{{
+
|* '''Max. {{#ifeq: {{{plane or copter?}}} |copter
#if:{{{max loading main|}}}
+
              | [[Disk loading|Disc loading]]
  |* '''Max disc loading:''' {{{max loading main|}}} ({{{max loading alt|}}})
+
              | [[wing loading]]
}}
+
            }}:''' {{{max loading main}}} ({{{max loading alt|}}})
|{{
 
#if:{{{max loading main|}}}
 
  |* '''Max [[wing loading]]:''' {{{max loading main|}}} ({{{max loading alt|}}})
 
}}
 
 
}}{{
 
}}{{
 
#switch:{{{jet or prop?}}}
 
#switch:{{{jet or prop?}}}
Line 213: Line 214:
 
   |{{
 
   |{{
 
   #if:{{{max thrust/weight|}}}
 
   #if:{{{max thrust/weight|}}}
   |* '''Minimum [[Thrust-to-weight ratio|thrust/weight]]:''' {{{max thrust/weight|}}}
+
   |* '''Minimum [[Thrust-to-weight ratio|thrust/weight]]:''' {{{max thrust/weight}}}
 
   }}
 
   }}
 
  }}
 
  }}
 
  |prop={{
 
  |prop={{
 
  #if:{{{max power/mass main|}}}
 
  #if:{{{max power/mass main|}}}
   |* '''Minimum [[Power-to-weight ratio|power/mass]]:''' {{{max power/mass main|}}} ({{{max power/mass alt|}}})
+
   |* '''Minimum [[Power-to-weight ratio|power/mass]]:''' {{{max power/mass main}}} ({{{max power/mass alt|}}})
 
  }}
 
  }}
 
  |both={{
 
  |both={{
 
  #if:{{{max power/mass main|}}}
 
  #if:{{{max power/mass main|}}}
   |* '''Minimum [[Power-to-weight ratio|power/mass]] (prop):''' {{{max power/mass main|}}} ({{{max power/mass alt|}}})
+
   |* '''Minimum [[Power-to-weight ratio|power/mass]] (prop):''' {{{max power/mass main}}} ({{{max power/mass alt|}}})
 
  }}{{
 
  }}{{
 
  #if:{{{max thrust/weight|}}}
 
  #if:{{{max thrust/weight|}}}
   |* '''Minimum [[Thrust-to-weight ratio|thrust/weight]] (jet):''' {{{max thrust/weight|}}}
+
   |* '''Minimum [[Thrust-to-weight ratio|thrust/weight]] (jet):''' {{{max thrust/weight}}}
 
  }}
 
  }}
 
  |
 
  |
}}
+
}}{{
{{{more performance|}}}{{
+
#if: {{{more performance|}}}|<nowiki />
#if:{{{armament|}}}{{{guns|}}}{{{bombs|}}}{{{missiles|}}}{{{rockets|}}}{{{hardpoints|}}}
+
{{{more performance|}}}
  |{{
+
}}{{
#if:{{{more performance|}}}
+
#if: {{{armament|}}}{{{guns|}}}{{{bombs|}}}{{{missiles|}}}{{{rockets|}}}{{{hardpoints|}}}
  |</ul>
+
  |<nowiki />
}}<h3>{{{armament header|Armament}}}<h3>
+
{{big|{{{armament header|'''Armament'''}}}}}<br />
 
{{{armament|{{
 
{{{armament|{{
#if:{{{guns|}}}{{{bombs|}}}{{{rockets|}}}{{{missiles|}}}{{{hardpoints|}}}
 
  |{{
 
 
   #if:{{{guns|}}}
 
   #if:{{{guns|}}}
   |* '''Guns:''' {{{guns}}}
+
   |* '''Guns:''' {{#if:1| {{{guns}}} }}
 
   }}{{
 
   }}{{
 
   #if:{{{hardpoints|}}}
 
   #if:{{{hardpoints|}}}
   |* '''Hardpoints:''' {{{hardpoints|}}} {{#if:{{{hardpoint capacity|}}}
+
   |* '''[[Hardpoint]]s:''' {{{hardpoints}}} {{#if:{{{hardpoint capacity|}}}
     |with a capacity of {{{hardpoint capacity|}}},
+
     |with a capacity of {{{hardpoint capacity}}}
 
   }}{{
 
   }}{{
 
   #if:{{{hardpoint rockets|}}}{{{hardpoint missiles|}}}{{{hardpoint bombs|}}}{{{hardpoint other|}}}
 
   #if:{{{hardpoint rockets|}}}{{{hardpoint missiles|}}}{{{hardpoint bombs|}}}{{{hardpoint other|}}}
     |with provisions to carry combinations of:
+
     |&nbsp;and provisions to carry combinations of:
 
   }}{{
 
   }}{{
 
   #if:{{{hardpoint rockets|}}}
 
   #if:{{{hardpoint rockets|}}}
Line 258: Line 257:
 
   }}{{
 
   }}{{
 
   #if:{{{hardpoint other|}}}
 
   #if:{{{hardpoint other|}}}
     |{{{hardpoint other}}}
+
     |** '''Other:''' {{{hardpoint other|}}}
 
   }}
 
   }}
 
   }}{{
 
   }}{{
Line 268: Line 267:
 
   }}{{
 
   }}{{
 
   #if:{{{bombs|}}}
 
   #if:{{{bombs|}}}
   |* '''Bombs:''' {{{bombs}}}
+
   |* '''Bombs:''' {{#if:1| {{{bombs}}} }}
  }}{{
+
   }}{{{other armament|}}}
   #if:{{{other armament|}}}
 
  |{{{other armament}}}
 
  }}</ul>
 
}}
 
 
}}}
 
}}}
 
}}{{
 
}}{{
#if:{{{avionics|}}}
+
#if: {{{avionics|}}}
  |{{
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  |<nowiki />
#if:{{{more performance|}}}
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{{big|{{{avionics header|'''Avionics'''}}}}}<br />
  |</ul>
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{{{avionics}}}
}}</ul><h3>Avionics<h3>
 
{{{avionics|}}}
 
 
}}<noinclude>
 
}}<noinclude>
=Instructions for use=
+
{{Documentation}}
__TOC__
 
This template has provisions for four sections: General characteristics, performance, armament, and avionics.  What follows is list of the parametres that appear in each section, and specialised instructions for their use where necessary.
 
 
 
Most numerical quantities are divided into 'main' and 'alt'.  For example, the quantity 'empty weight' is specified by the parametres {{{emtpy weight main}}} and {{{empty weight alt}}}.  For a U.S. aircraft, which are measured using the [[Imperial unit|Imperial System of units]], the value for 'main' would be given in pounds (lb), and the value for 'alt' in kilograms (kg).  Most other aircraft are measured using the [[Metric system]], so they will have kg for 'main' and lb for 'alt'.
 
 
 
Because of the [[m:ParserFunctions|ParserFunctions]] this template uses, all values will automatically appear in the article once they have been specified.  For example, if I specify <code>|area main=1,000 ft²|area alt=93 m²</code>, the text
 
* '''Wing area:''' 1,000 ft² (93 m²)
 
will automatically appear in the article.
 
 
 
In the following instructions, parametres are referred to thus: {{{parametre name}}}.  When indicating which values should be entered for each parametre, the notation <code>|parametre name=vale</code> will be used.
 
 
 
==Non-specifications parametres==
 
The template uses three paramtres that are not directly related to the specs: {{{plane or copter?}}}, {{{jet or prop?}}}, and {{{ref}}}.  The first two control template output; the last one provides citation information.
 
;{{{plane or copter?}}}:If the aircraft is a rotorcraft (including helicopters, gyrodynes, tiltrotors, etc.), the value for this parametre should be <code>|plane or copter?=copter</code>.  If it is a fixed wing aircraft, the value should be specified as <code>|plane or copter?=plane</code>.
 
;{{{jet or prop?}}}:For planes that are powered by jet engines or rockets, specify <code>|jet or prop?=jet</code>. For those powered by propellers, specify <code>|jet or prop?=prop</code>.  Occasionally, aircraft have both jet engines and propellers; for these, specify <code>|jet or prop?=both</code>.  Unpowered aircraft such as gliders should be denoted by <code>|jet or prop?=neither</code>.
 
;{{{ref}}}:Used to cite the sources for the specifications section.  Example: <code><nowiki>|ref=The Encyclopedia of World Aircraft&lt;ref>{{cite encyclopedia|last=Donald|first=David|year=1997|title=Boeing Model 299 (B-17 Flying Fortress|encyclopedia=The Encyclopedia of World Aircraft: 1|location=Etobicoke, Ontario, Canada|publisher=Prospero Books|id=ISBN 1-85605-375-X|pages=pages 154-155}}</ref></nowiki></code>.  See [[Wikipedia:Citation templates]] for information on the citation templates available and how to use them.
 
 
 
==General characteristics==
 
;{{{crew}}}:The number of people required to operate the aircraft.  If you wish to specify the roles played by each crew member, do so in something similar to the following format: <code>|crew=3 (pilot, copilot, flight engineer)</code>
 
;{{{capacity}}}:The number of passengers the aircraft can carry.  For civilian passenger aircraft, this should usually be specified <var>x</var> number of passengers: <code>|capacity=88 passengers</code>.  Most military transports can be used for patients.  In this case, something similar to the system used for the C-130 Hercules may be in order:
 
<pre>|capacity=<br/>
 
** 92 passengers ''or''
 
** 64 airborne troops ''or''
 
** 74 litter patients with 2 medical personnel
 
</pre>
 
;{{{payload main}}}, {{{payload alt}}}, {{{payload more}}}:Specifies the amount of cargo that can be carried by an aircraft.  For 'main' and 'alt', specify the weight of the payload.  If applicable, use {{{payload more|}}} to specify the type of payload usually carried, such as fertiliser for agricultural aircraft or mail for mailplanes.
 
;{{{length main}}}, {{{length alt}}}:The length of the aircraft from nose to tail.  For helicopters, this means the length of the fuselage without taking the rotor into consideration.
 
;{{{span main}}}, {{{span alt}}}:The wingspan of fixed wing aircraft, or the main rotor diameter for rotorcraft.
 
;{{{height main}}}, {{{height alt}}}
 
;{{{area main}}}, {{{area alt}}}:The area of the wing of a fixed wing aircraft, or the total area of all main rotors for rotorcraft (does not include maneuvering rotors).
 
;{{{airfoil}}}:For fixed wing aircraft, the type of airfoil the wing uses. Eg, see [[NACA airfoil]] for information on airfoil types.
 
;{{{empty weight main}}}, {{{empty weight alt}}}:The weight of the aircraft when unloaded—no crew, passengers, cargo, or fuel.
 
;{{{loaded weight main}}}, {{{loaded weight alt}}}:The weight of the aircraft when loaded for a 'typical' mission.  This statistic is cited for almost any aircraft, but it is relatively arbitrary, so only use statistics given in sources.
 
;{{{useful load main}}}, {{{useful load alt}}}:The difference between the aircraft's maximum weight and empty weight.
 
;{{{max takeoff weight main}}}, {{{max takeoff weight alt}}}, {{{max takeoff weight more}}}:The heaviest the aircraft can be and still get off the ground.
 
;{{{more general}}}: A place to put anything relevant not included already under the general parameters eg "Fuel Capacity: 500 gallons"
 
 
 
==Engines==
 
If there is any information that needs to be added after the engine specs, it should be added using the parameter {{{more general}}}.
 
 
 
===Propellers===
 
;{{{number of props}}}:The number of engines that drive the propellers.  For fixed wing aircraft, this is usually—but not always—the same as the number of propellers.
 
;{{{engine (prop)}}}:The model of engine the aircraft uses.  Example: <code><nowiki>|engine (prop)=[[Pratt & Whitney R-4360]]-53 "Wasp Major"</nowiki></code>.
 
;{{{type of prop}}}:The configuration of the engine.  Examples: <code><nowiki>|type of prop=liquid-cooled [[V12 engine]]</nowiki></code>, <code><nowiki>|type of prop=[[turboprop]]</nowiki></code>, <code><nowiki>|type of prop=[[radial engine]]</nowiki></code>.
 
;{{{power main}}}, ({{{power alt}}}):The power output of the engine.
 
;{{{power original}}}:For some engines the power output may have been originally measured in an unconventional unit.  For example, older German engines originally had their power measured in [[Pferdestärke]] (PS).  Sample usage of this parametre: <code><nowiki>|power original=<ref>Originally measured as 15,000 [[Pferdestärke|PS]].</nowiki></code>
 
;{{{power more}}}:More information on the power rating, such as the rpm of the engine.
 
 
 
===Jets===
 
;{{{number of jets}}}:The number of jet engines or rockets the aircraft has.
 
;{{{engine (jet)}}}:The model of jet or rocket used by the aircraft
 
;{{{type of jet}}}:The configuration of jet, such as [[turbojet]], [[turbofan]], [[thermojet]], [[rocket]], etc.
 
;{{{afterburning thrust main}}}, {{{afterburning thrust alt}}}:Thrust of the engine with afterburner, if applicable.
 
;{{{thrust main}}}, {{{thrust alt}}}:The thrust of the engine; if the engine has afterburners, this parametre denotes dry thrust.
 
;{{{afterburning thrust original}}}, {{{thrust original}}}:Some engines had their original measurements taken in unconventional units.  For example, many Russian and Soviet engines were originally rated using [[kilogram-force]].
 
 
 
===Propeller model and configuration===
 
;{{{propeller or rotor?}}}:If it is a propeller on a fixed wing aircraft, specify <code>|propeller or rotor?=propeller</code>.  If it is a rotor on a helicopter or other rotary wing aircraft, specify <code>|propeller or rotor=rotor</code>.
 
;{{{propellers}}}:The model and configuration of the propellers.  Example: <code><nowiki>|propellers=Three-bladed [[Hamilton Standard]]</nowiki></code>.
 
;{{{number of propellers per engine}}}:With some aircraft, multiple propellers will be driven off one engine.  Use this parametre to specify the number per engine.
 
;{{{propeller diameter main}}}, {{{propeller diameter alt}}}:Used to indicate the diameter of the propellers.  For helicopters, the rotor diameter was already specified using the {{{span}}} parameter.
 
 
 
==Performance==
 
Will be added later.
 
 
 
==Armament==
 
do not use <code>|armament=</code>
 
 
 
at all (even with a blank entry) but instead use
 
 
 
<code>|guns= </code><br/>
 
<code>|bombs= </code><br/>
 
<code>|rockets= </code><br/>
 
<code>|missiles= </code><br/>
 
<code>|hardpoints= </code><br/>
 
<code>|hardpoint capacity= </code>
 
 
 
to specify capacity of hardpoints.
 
 
 
==Avionics==
 
Will be added later
 
 
 
[[ja:Template:航空機スペック]]
 
[[es:Plantilla:Especificaciones de aeronave]]
 
 
</noinclude>
 
</noinclude>

Latest revision as of 13:36, 18 October 2020

General characteristics

Performance

Template documentation[view] [edit] [history] [purge]

Usage

{{aircraft specifications
<!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]]. -->
| plane or copter? = <!-- options: plane/copter -->
| jet or 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 does not apply, like capacity, leave it blank. 
-->
| ref = 
<!--  General characteristics  -->
| crew         = 
| capacity     = 
| payload main = 
| payload alt  = 
| payload more = 
| length main  = 
| length alt   = 
| span main    = 
| span alt     = 
| height main  = 
| height alt   = 
| area main    = 
| area alt     = 
| airfoil      = 
| aspect ratio = 
| empty weight main  = 
| empty weight alt   = 
| useful load main   = 
| useful load alt    = 
| loaded weight main = 
| loaded weight alt  = 
| max takeoff weight main = 
| max takeoff weight alt  = 
| more general            = 
<!--  Powerplant, jet engine(s)  -->
| engine (jet)    = 
| type of jet     = 
| number of jets  = 
| thrust main     = 
| thrust alt      = 
| thrust original = 
| afterburning thrust main = 
| afterburning thrust alt  = 
<!--  Powerplant, prop(s)  -->
| engine (prop)   = 
| type of prop    = 
| number of props = 
| power main      = 
| power alt       = 
| power original  = 
<!--  Powerplant, propellor/rotor details  -->
| propeller or rotor?     = <!-- options: propeller/rotor -->
| propellers              = 
| number of propellers per engine = 
| propeller diameter main = 
| propeller diameter alt  = 

| more general powerplant =
<!-- Performance  -->
| max speed main    = 
| max speed alt     = 
| max speed more    = 
| cruise speed main = 
| cruise speed alt  = 
| cruise speed more = 
| stall speed main  = 
| stall speed alt   = 
| stall speed more  = 
| never exceed speed main = 
| never exceed speed alt  = 
| range main        = 
| range alt         = 
| range more        = 
| combat radius main= 
| combat radius alt = 
| combat radius more= 
| ferry range main  = 
| ferry range alt   = 
| ferry range more  = 
| endurance         = 
| ceiling main      = 
| ceiling alt       = 
| ceiling more      = 
| climb rate main   = 
| climb rate alt    = 
| climb rate more   = 
| sink rate main    = 
| sink rate alt     = 
| sink rate more    = 
| loading main      = 
| loading alt       = 
| thrust/weight     = 
| power/mass main   = 
| power/mass alt    = 
| more performance  = 
<!--  Armament  -->
| armament = <!-- If you want to use the following specific parameters, do not use this line at all -->
| guns     = 
| bombs    = 
| rockets  = 
| missiles = 
 
| hardpoints = 
| hardpoint capacity = 
| hardpoint rockets  = 
| hardpoint missiles = 
| hardpoint bombs    = 
| hardpoint other    = 

| avionics = 

}}

Aircraft specifications

Editors beware: formatting of code to make it "look nice" is very likely to inadvertently introduce leading and trailing blank lines into the template output.

This template has provisions for four sections: General characteristics, performance, armament, and avionics. What follows is list of the parameters that appear in each section, and specialised instructions for their use where necessary.

Most numerical quantities are divided into 'main' and 'alt'. For example, the quantity 'empty weight' is specified by the parameters {{{empty weight main}}} and {{{empty weight alt}}}. The choice of which is the given first will depend on origin and period. A U.S. aircraft would have U.S. System of customary units given first (in the example of weight 'main' would be given in pounds (lb), and the value for 'alt' in kilograms (kg). Other aircraft are measured using the metric system, so they will have kg for 'main' and lb for 'alt'. Prior to the adoption of metric units, British aircraft used Imperial units, and RAF aircraft used mph until after WWII while Fleet Air Arm aircraft used knots.

Because of the ParserFunctions this template uses, all values will automatically appear in the article once they have been specified. For example, if I specify |area main=1,000 ft<sup>2</sup>|area alt=93 m<sup>2</sup>, the text

  • Wing area: 1,000 ft2 (93 m2)

will automatically appear in the article.

In the following instructions, parameters are referred to thus: {{{parameter name}}}. When indicating which values should be entered for each parameter, the notation |parameter name=vale will be used.

Non-specifications parameters

The template uses three paramters that are not directly related to the specs: {{{plane or copter?}}}, {{{jet or prop?}}}, and {{{ref}}}. The first two control template output; the last one provides citation information.

{{{plane or copter?}}}
If the aircraft is a rotorcraft (including helicopters, gyrodynes, tiltrotors, etc.), the value for this parameter should be |plane or copter?=copter. If it is a fixed wing aircraft, the value should be specified as |plane or copter?=plane.
{{{jet or prop?}}}
For planes that are powered by jet engines or rockets, specify |jet or prop?=jet. For those powered by propellers, specify |jet or prop?=prop. Occasionally, aircraft have both jet engines and propellers; for these, specify |jet or prop?=both. Unpowered aircraft such as gliders should be denoted by |jet or prop?=neither.
{{{ref}}}
Used to cite the sources for the specifications section. Example: |ref=The Encyclopedia of World Aircraft<ref>{{cite encyclopedia|last=Donald|first=David|year=1997|title=Boeing Model 299 (B-17 Flying Fortress|encyclopedia=The Encyclopedia of World Aircraft: 1|location=Etobicoke, Ontario, Canada|publisher=Prospero Books| ISBN =1-85605-375-X|pages=pages 154-155}}</ref>. See Wikipedia:Citation templates for information on the citation templates available and how to use them.

General characteristics

{{{crew}}}
The number of people required to operate the aircraft. If you wish to specify the roles played by each crew member, do so in something similar to the following format: |crew=3 (pilot, copilot, flight engineer)
{{{capacity}}}
The number of passengers the aircraft can carry if the plane is commercial. For general aviation aircraft, this should usually be specified x number of passengers: |capacity=88 passengers and can include crew. Most military transports can be used for patients. In this case, something similar to the system used for the C-130 Hercules may be in order:
|capacity=<br/>
** 92 passengers ''or''
** 64 airborne troops ''or''
** 74 litter patients with 2 medical personnel
{{{payload main}}}, {{{payload alt}}}, {{{payload more}}}
Specifies the amount of cargo that can be carried by an aircraft. For 'main' and 'alt', specify the weight of the payload. If applicable, use to specify the type of payload usually carried, such as fertiliser for agricultural aircraft or mail for mailplanes.
{{{length main}}}, {{{length alt}}}
The length of the aircraft from nose to tail. For helicopters, this means the length of the fuselage without taking the rotor into consideration.
{{{span main}}}, {{{span alt}}}
The wingspan of fixed wing aircraft, or the main rotor diameter for rotorcraft.
{{{height main}}}, {{{height alt}}}
{{{area main}}}, {{{area alt}}}
The area of the wing of a fixed wing aircraft, or the total area of all main rotors for rotorcraft (does not include maneuvering rotors).
{{{airfoil}}}
For fixed wing aircraft, the type of airfoil the wing uses. Eg, see NACA airfoil for information on airfoil types.
aspect ratio
for fixed wing aircraft, the aspect ratio of the wing - a parameter generally of interest in gliders (sailplanes)
{{{empty weight main}}}, {{{empty weight alt}}}
The weight of the aircraft when unloaded—no crew, passengers, cargo, or fuel.
{{{loaded weight main}}}, {{{loaded weight alt}}}
The weight of the aircraft when loaded for a 'typical' mission. This statistic is cited for almost any aircraft, but it is relatively arbitrary, so only use statistics given in sources.
{{{useful load main}}}, {{{useful load alt}}}
The difference between the aircraft's maximum weight and empty weight.
{{{max takeoff weight main}}}, {{{max takeoff weight alt}}}, {{{max takeoff weight more}}}
The heaviest the aircraft can be and still get off the ground.
{{{more general}}}
A place to put anything relevant not included already under the general parameters e.g. "Fuel Capacity: 500 gallons"

Engines

If there is any information that needs to be added after the engine specs, it should be added using the parameter {{{more general powerplant}}}. eg |more general powerplant=engines coupled through gearbox.

Propeller driven aircraft

{{{number of props}}}
The number of engines that drive the propellers. For fixed wing aircraft, this is usually—but not always—the same as the number of propellers.
{{{engine (prop)}}}
The model of engine the aircraft uses. Example: |engine (prop)=[[Pratt & Whitney R-4360]]-53 "Wasp Major".
{{{type of prop}}}
The configuration of the engine. Examples: |type of prop=liquid-cooled [[V12 engine]], |type of prop=[[turboprop]], |type of prop=[[radial engine]].
{{{power main}}}, ({{{power alt}}})
The power output of the engine.
{{{power original}}}
For some engines the power output may have been originally measured in an unconventional unit. For example, older German engines originally had their power measured in Pferdestärke (PS). Sample usage of this parameter: |power original=<ref>Originally measured as 15,000 [[Pferdestärke|PS]].
{{{power more}}}
More information on the power rating, such as the rpm of the engine.

Jet aircraft

{{{number of jets}}}
The number of jet engines or rockets the aircraft has.
{{{engine (jet)}}}
The model of jet or rocket used by the aircraft
{{{type of jet}}}
The configuration of jet, such as turbojet, turbofan, thermojet, rocket, etc.
{{{afterburning thrust main}}}, {{{afterburning thrust alt}}}
Thrust of the engine with afterburner, if applicable.
{{{thrust main}}}, {{{thrust alt}}}
The thrust of the engine; if the engine has afterburners, this parameter denotes dry thrust.
{{{afterburning thrust original}}}, {{{thrust original}}}
Some engines had their original measurements taken in unconventional units. For example, many Russian and Soviet engines were originally rated using kilogram-force.

Propeller model and configuration

{{{propeller or rotor?}}}
If it is a propeller on a fixed wing aircraft, specify |propeller or rotor?=propeller. If it is a rotor on a helicopter or other rotary wing aircraft, specify |propeller or rotor=rotor.
{{{propellers}}}
The model and configuration of the propellers. Example: |propellers=Three-bladed [[Hamilton Standard]].
{{{number of propellers per engine}}}
With some aircraft, multiple propellers will be driven off one engine. Use this parameter to specify the number per engine.
{{{propeller diameter main}}}, {{{propeller diameter alt}}}
Used to indicate the diameter of the propellers. For helicopters, the rotor diameter was already specified using the {{{span}}} parameter.

Performance

The available parameter fields are: Their use is fairly obvious.

  • | never exceed speed main =
  • | never exceed speed alt =
  • | never exceed speed more =
  • | max speed main =
  • | max speed alt =
  • | max speed more = (displays only when there is a value for max speed alt )
  • | cruise speed main =
  • | cruise speed alt =
  • | cruise speed more =
  • | stall speed main =
  • | stall speed alt =
  • | stall speed more =
  • | lift to drag =
  • | minimum control speed main =
  • | minimum control speed alt =
  • | minimum control speed more =
  • | range main =
  • | range alt =
  • | range more =
  • | combat radius main =
  • | combat radius alt =
  • | combat radius more =
  • | ferry range main =
  • | ferry range alt =
  • | ferry range more =
  • | endurance = (patrol aircraft and older aircraft may have this instead of range)
  • | ceiling main =
  • | ceiling alt =
  • | ceiling more =
  • | climb rate main =
  • | climb rate alt =
  • | climb rate more =
  • | sink rate main =
  • | sink rate alt =
  • | sink rate more =
  • | fuel consumption =
  • | performance more =

Armament

You can use |armament= followed by a bulletted list of the armaments, or omit that line entirely and use the following specific parameters. If you include the line |armament= at all—even with an empty value—then none of the following parameters will have any effect.

| guns =
| bombs =
| rockets =
| missiles =
| hardpoints = to specify the number of hardpoints
| hardpoint capacity = to specify the capacity of hardpoints eg as total payload
and
| hardpoint rockets =
| hardpoint missiles=
| hardpoint bombs =
| hardpoint other =

to specify the types of hardpoint weapons

Avionics

Will be added later