Difference between revisions of "Template:Infobox/Part/jet engine"

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<includeonly>{{Partbox|name={{{name|}}}|role={{lang|en=Liquid Fuel Engine|pl=Silnik na paliwo ciekłe}}|class=LiquidEngine|file={{{file|}}}|size={{{size|}}}|size2={{{size2|}}}|costs={{{costs}}}|mass={{{mass}}}|drag={{{drag}}}|temp={{{temp}}}|tolerance={{{tolerance}}}|manufacturer={{{manufacturer|}}}|since={{{since}}}|part={{{part}}}|more=
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<noinclude>{{Infobox/Part/preview|
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{{Partbox/Line|{{Partbox/Dict|Maximum thrust}}|{{{thrust}}}&nbsp;kN}}
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</noinclude>{{Infobox/Part/Thrust|{{{thrust<noinclude>|100</noinclude>}}}}}
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{{Partbox/Line|Stall Threshold|{{{stall}}}&nbsp;kN}}
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{{Infobox/Part/ISP|{{{isp<noinclude>|2000</noinclude>}}}|where=max}}
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{{Partbox/Line|{{lang|en=Optimal Airflow|pl=Optymalny przepływ powietrza}}|{{{opt-air}}}}}
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{{Infobox/Part/consumption|5000|{{{thrust<noinclude>|100</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}|{{mark|fuelu}}|2}}
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{{Partbox/Line|{{lang|en=Intake Size|pl=Rozmiar wlotu}}|{{{in-size}}}}}
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{{Infobox/Part/consumption|5000|{{{thrust<noinclude>|100</noinclude>}}}*{{{intake<noinclude>|22</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}|{{mark|airu}}|2|{{Infobox/Part/Dict|Consumption-air}}}}
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{{Partbox/Line|{{lang|en=Intake Power|pl=Moc ssania}}|{{{in-pow}}}}}
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{{Infobox/Part/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|<noinclude>2.5</noinclude>}}}|{{{vectoring<noinclude>|2.5</noinclude>}}}&nbsp;°|{{No}}}}}}<noinclude>
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{{Partbox/FuelConsumption/Cell|5000|{{{fuel}}}}}
 
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{{Partbox/Line|{{Partbox/Dict|Vectoring}}|{{#if: {{{vectoring|}}}|{{{vectoring}}}&nbsp;°|No}}}}}}</includeonly><noinclude>{{Partbox/JetEngine
 
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|name=Basic Jet Engine
 
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|file=Basicjetengine.png
 
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|costs=950
 
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|mass=1
 
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|drag=0.2
 
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|temp=3600
 
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|tolerance=7
 
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|manufacturer=
 
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|thrust=100
 
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|stall=20
 
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|opt-air=200
 
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|in-size=1.1
 
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|in-pow=125
 
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|fuel=0.3
 
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|vectoring=2.5
 
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|since=v0.15
 
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|part=JetEngine
 
 
}}
 
}}
  
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{{Tl|Partbox}} implementation for jet engines.
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{{Tl|Infobox/Part}} modules for [[jet engine]]s. It uses {{Tl|Infobox/Part/Thrust}}, {{Tl|Infobox/Part/ISP}} and {{Tl|Infobox/Part/consumption}}. Other engine types:
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* [[Liquid fuel engine]]s: {{Tl|Infobox/Part/reaction engine}}
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* [[Solid rocket booster]]s: {{Tl|Infobox/Part/solid fuel engine}} (uses reaction engine template)
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* [[Ion engine]]s: {{Tl|Infobox/Part/ion engine}} (uses reaction engine template)
  
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== Parameters ==
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{{Parameter table|name=text|parameters=
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{{Partbox/Parameters|additional=
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{{Parameter row|thrust|Maximum thrust in kN}}
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{{ParameterRow|thrust|Maximum Thrust}}
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{{Parameter row|isp|The maximum specific impulse}}
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{{ParameterRow|stall|Stall Threshold}}
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{{Parameter row|intake|The amount of IntakeAir is needed}}
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{{ParameterRow|opt-air|Optimal Airflow}}
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{{Parameter row|vectoring|Thrust vectoring, if not set displays “No”.|Not set/No}}
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{{ParameterRow|in-size|Intake Size}}
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}}
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{{ParameterRow|in-pow|Intake Power}}
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{{Subcategory|modules}}</noinclude>
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{{ParameterRow|fuel|Fuel Consumption}}
 
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{{ParameterRow|vectoring|Thrust Vectoring|Not set/No}}}}
 
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[[Category:Templates|Partbox/JetEngine]]</noinclude>
 

Latest revision as of 16:20, 11 September 2024

Maximum thrust 100.00 kN
Isp (max) 2000 s
Fuel consumption 1.02 Units of fuel/s
Intake air consumption 22.43 Air unit/s
Thrust vectoring 2.5 °

{{Infobox/Part}} modules for jet engines. It uses {{Infobox/Part/Thrust}}, {{Infobox/Part/ISP}} and {{Infobox/Part/consumption}}. Other engine types:

Name Optional Description Default
thrust No Maximum thrust in kN
isp No The maximum specific impulse
intake No The amount of IntakeAir is needed
vectoring Yes Thrust vectoring, if not set displays “No”. Not set/No
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