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

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m (+link to thrust vectoring;)
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<includeonly>{{Infobox/Part|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}}}|parent=Engine|more=
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<noinclude>{{Infobox/Part/preview|
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{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust}}}&nbsp;kN}}
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</noinclude>{{Infobox/Part/Thrust|{{{thrust<noinclude>|100</noinclude>}}}}}
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{{Infobox/Line|{{lang|en=Stall Threshold}}|{{{stall}}}&nbsp;kN}}
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{{Infobox/Part/ISP|{{{isp<noinclude>|2000</noinclude>}}}|where=max}}
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{{Infobox/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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{{Infobox/Line|{{lang|en=[[Intake air]] 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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{{Infobox/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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{{Infobox/Part/FuelConsumption/Cell|5000|{{{fuel}}}}}
 
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{{Infobox/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|}}}|{{{vectoring}}}&nbsp;°|No}}}}}}</includeonly><noinclude>{{Infobox/Part/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|Infobox/Part}} 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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{{Infobox/Part/Sub|additional=
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{{Parameter table|name=text|parameters=
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{{Parameter Row|thrust|Maximum Thrust}}
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{{Parameter row|thrust|Maximum thrust in kN}}
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{{Parameter Row|stall|Stall Threshold}}
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{{Parameter row|isp|The maximum specific impulse}}
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{{Parameter Row|opt-air|Optimal Airflow}}
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{{Parameter row|intake|The amount of IntakeAir is needed}}
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{{Parameter Row|in-size|Intake air size}}
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{{Parameter row|vectoring|Thrust vectoring, if not set displays “No”.|Not set/No}}
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{{Parameter Row|in-pow|Intake power}}
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}}
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{{Parameter Row|fuel|Fuel Consumption}}
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{{Subcategory|modules}}</noinclude>
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{{Parameter Row|vectoring|Thrust Vectoring|Not set/No}}}}</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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