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Template:Aircraft specifications: Difference between revisions

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Template:Aircraft specifications (edit)

Revision as of 00:35, 27 May 2017

160 bytes added ,  6 years ago
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(Created page with "{{ #if: {{{ref|}}} |<p style="font-size: 90%; margin:0; padding: .2em">''Data from'' {{{ref}}}</p> }}<span style="font-size: 120%;">'''General characteristics'''</span>{{ #if...")
 
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Line 10:
}}{{
#if: {{{payload main|}}}
|* '''[[{{wpl|Payload]]}}:''' {{{payload main}}} ({{{payload alt|}}}) {{{payload more|}}}
}}
* '''Length:''' {{{length main|}}} ({{{length alt|}}})
* '''{{#ifeq: {{{plane or copter?}}} | copter
|Rotor diameter
|[[{{wpl|Wingspan]]}}
}}:''' {{{span main|}}} ({{{span alt|}}})
* '''Height:''' {{{height main|}}} ({{{height alt|}}}){{
Line 26:
}}{{
#if: {{{airfoil|}}}
|* '''[[{{wpl|Airfoil]]}}:''' {{{airfoil}}}
}}{{
#if: {{{aspect ratio|}}}
|* '''[[{{wpl|Aspect ratio (aeronautics)|Aspect ratio]]}}:''' {{{aspect ratio}}}
}}{{
#if: {{{empty weight main|}}}
|* '''[[{{wpl|Manufacturer's empty weight|Empty weight]]}}:''' {{{empty weight main|}}} ({{{empty weight alt|}}})
}}{{
#if: {{{useful load main|}}}
Line 41:
}}{{
#if: {{{max takeoff weight main|}}}
|* '''[[{{wpl|Maximum takeoff weight|Max. takeoff weight]]}}:''' {{{max takeoff weight main}}} ({{{max takeoff weight alt|}}}) {{{max takeoff weight more|}}}
}}{{
#if: {{{more general|}}}
Line 47:
}}{{
#switch: {{{jet or prop?}}}
|prop =* '''[[{{wpl|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
Line 60:
|{{ #if: {{{propellers|}}} |**|*}} '''Propeller diameter:''' {{{propeller diameter main}}} ({{{propeller diameter alt|}}})
}}
| jet =* '''[[{{wpl|Aircraft engine|Powerplant]]}}:''' {{{number of jets|}}} × {{{engine (jet)|}}} {{{type of jet|}}}{{
#if: {{{thrust main|}}}
|{{
Line 69:
|each
}}
** '''Thrust with [[{{wpl|afterburner]]}}:''' {{{afterburning thrust main}}} ({{{afterburning thrust alt|}}}) {{{afterburning thrust original|}}} <!--
 
follows ELSE branch of if [NOT] afterburning
Line 79:
|each }}
}}
|both=* '''[[{{wpl|Aircraft engine|Powerplant]]}}:'''
** {{{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
Line 110:
{{
#if: {{{never exceed speed main|}}}
|* '''[[{{wpl|V speeds#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|}}}
|* '''[[{{wpl|V speeds#Regulatory_V-speeds|Maximum speed]]}}:''' {{{max speed main}}} {{
#if:{{{max speed alt|}}}
|({{{max speed alt}}}) {{{max speed more|}}}
Line 121:
}}{{
#if:{{{cruise speed main|}}}
|* '''[[{{wpl|V speeds#Vc|Cruise speed]]}}:''' {{{cruise speed main|}}} {{
#if:{{{cruise speed alt|}}}
|({{{cruise speed alt|}}}) {{{cruise speed more|}}}
Line 127:
}}{{
#if: {{{stall speed main|}}}
|* '''[[{{wpl|Stall (fluid mechanics)#Stall speed|Stall speed]]}}:''' {{{stall speed main}}} ({{{stall speed alt|}}}) {{{stall speed more|}}}
}}{{
#if: {{{minimum control speed main|}}}
|* '''[[{{wpl|V speeds#Vmc|Minimum controllable speed]]}}:''' {{{minimum control speed main}}} ({{{minimum control speed alt|}}}) {{{minimum control speed more|}}}
}}{{
#if:{{{range main|}}}
|* '''[[{{wpl|Range (aeronautics)|Range]]}}:''' {{{range main}}} ({{{range alt|}}}) {{{range more|}}}
}}{{
#if:{{{combat radius main|}}}
|* '''[[{{wpl|Combat radius]]}}:''' {{{combat radius main}}} ({{{combat radius alt|}}}) {{{combat radius more|}}}
}}{{
#if:{{{combat range main|}}}
Line 142:
}}{{
#if:{{{ferry range main|}}}
|* '''[[{{wpl|Range (aeronautics)|Ferry range]]}}:''' {{{ferry range main}}} ({{{ferry range alt|}}}) {{{ferry range more|}}}
}}{{
#if: {{{endurance|}}}
|* '''[[{{wpl|Endurance (aeronautics)|Endurance]]}}:''' {{{endurance}}}
}}{{
#if: {{{ceiling main|}}}
|* '''[[{{wpl|Ceiling (aeronautics)|Service ceiling]]}}:''' {{{ceiling main}}} ({{{ceiling alt|}}}) {{{ceiling more|}}}
}}{{
#if: {{{climb rate main|}}}
|* '''[[{{wpl|Rate of climb]]}}:''' {{{climb rate main}}} ({{{climb rate alt|}}}) {{{climb rate more|}}}
}}{{
#if: {{{sink rate main|}}}
|* '''[[{{wpl|Rate of climb|sink rate]]}}:''' {{{sink rate main}}} ({{{sink rate alt|}}}) {{{sink rate more|}}}
}}{{
#if: {{{glide ratio|}}}
|* '''[[{{wpl|Gliding flight#Glide ratio|Glide ratio]]}}:''' {{{glide ratio}}}
}}{{
#if: {{{loading main|}}}
|* '''{{#ifeq: {{{plane or copter?}}} |copter
|[[{{wpl|Disk loading|Disc loading]]}}
|[[{{wpl|Wing loading]]}}
}}:''' {{{loading main}}} ({{{loading alt|}}})
}}{{
#if:{{{lift to drag|}}}
|* '''[[{{wpl|Lift-to-drag ratio|lift-to-drag]]}}:''' {{{lift to drag}}}
}}{{
#if:{{{fuel consumption|}}}
|* '''[[{{wpl|Fuel efficiency|Fuel consumption]]}}:''' {{{fuel consumption}}}
}}{{
#switch: {{{jet or prop?}}}
|jet={{ #if: {{{afterburning thrust/weight|}}}
|* '''[[{{wpl|Thrust-to-weight ratio|Thrust/weight]]:'''{{
#if:{{{thrust/weight|}}}
|** '''Dry:''' {{{thrust/weight}}}
Line 180:
|{{
#if:{{{thrust/weight|}}}
|* '''[[{{wpl|Thrust-to-weight ratio|Thrust/weight]]}}:''' {{{thrust/weight}}}
}}
}}
|prop={{
#if:{{{power/mass main|}}}
|* '''[[{{wpl|Power-to-weight ratio|Power/mass]]}}:''' {{{power/mass main}}} ({{{power/mass alt|}}})
}}
|both={{
#if:{{{power/mass main|}}}
|* '''[[{{wpl|Power-to-weight ratio|Power/mass]]}} (prop):''' {{{power/mass main}}} ({{{power/mass alt|}}})
}}{{
#if:{{{thrust/weight|}}}
|* '''[[{{wpl|Thrust-to-weight ratio|Thrust/weight]]}} (jet):''' {{{thrust/weight}}}
}}
}}{{
#if: {{{max loading main|}}}
|* '''Max. {{#ifeq: {{{plane or copter?}}} |copter
| [[{{wpl|Disk loading|Disc loading]]}}
| [[{{wpl|wing loading]]}}
}}:''' {{{max loading main}}} ({{{max loading alt|}}})
}}{{
#switch:{{{jet or prop?}}}
|jet={{#if:{{{max afterburning thrust/weight|}}}
|* '''Minimum [[{{wpl|Thrust-to-weight ratio|thrust/weight]]}}:'''{{
#if:{{{max thrust/weight|}}}
|** '''Dry:''' {{{max thrust/weight|}}}
Line 210:
|{{
#if:{{{max thrust/weight|}}}
|* '''Minimum [[{{wpl|Thrust-to-weight ratio|thrust/weight]]}}:''' {{{max thrust/weight}}}
}}
}}
|prop={{
#if:{{{max power/mass main|}}}
|* '''Minimum [[{{wpl|Power-to-weight ratio|power/mass]]}}:''' {{{max power/mass main}}} ({{{max power/mass alt|}}})
}}
|both={{
#if:{{{max power/mass main|}}}
|* '''Minimum [[{{wpl|Power-to-weight ratio|power/mass]]}} (prop):''' {{{max power/mass main}}} ({{{max power/mass alt|}}})
}}{{
#if:{{{max thrust/weight|}}}
|* '''Minimum [[{{wpl|Thrust-to-weight ratio|thrust/weight]]}} (jet):''' {{{max thrust/weight}}}
}}
|
Line 239:
}}{{
#if:{{{hardpoints|}}}
|* '''[[{{wpl|Hardpoint]]}}s:''' {{{hardpoints}}} {{#if:{{{hardpoint capacity|}}}
|with a capacity of {{{hardpoint capacity}}}
}}{{
Retrieved from "https://en.omniversalis.org/wiki/Special:MobileDiff/546"