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

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m (+link to thrust vectoring;)
(*change to module;)
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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=
+
<noinclude>{{Infobox/Part/preview|</noinclude>
{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust}}}&nbsp;kN}}
+
{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust<noinclude>|100</noinclude>}}}&nbsp;kN}}
{{Infobox/Line|{{lang|en=Stall Threshold}}|{{{stall}}}&nbsp;kN}}
+
{{Infobox/Line|{{lang|en=Stall Threshold}}|{{{stall<noinclude>|10</noinclude>}}}&nbsp;kN}}
{{Infobox/Line|{{lang|en=Optimal Airflow|pl=Optymalny przepływ powietrza}}|{{{opt-air}}}}}
+
{{Infobox/Part/ISP|{{{isp<noinclude>|2000</noinclude>}}}}}
{{Infobox/Line|{{lang|en=[[Intake air]] size|pl=Rozmiar wlotu}}|{{{in-size}}}}}
+
{{Infobox/Part/FuelConsumption|5000|{{{thrust<noinclude>|100</noinclude>}}}/16|{{{isp<noinclude>|100</noinclude>}}}||l|2}}
{{Infobox/Line|{{lang|en=Intake power|pl=Moc ssania}}|{{{in-pow}}}}}
+
{{Infobox/Part/FuelConsumption|5000|{{{thrust<noinclude>|100</noinclude>}}}/16*15|{{{isp<noinclude>|100</noinclude>}}}||l|2|Intake air consumption}}
{{Infobox/Part/FuelConsumption/Cell|5000|{{{fuel}}}}}
+
{{Infobox/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|<noinclude>2.5</noinclude>}}}|{{{vectoring<noinclude>|2.5</noinclude>}}}&nbsp;°|{{No}}}}}}
{{Infobox/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|}}}|{{{vectoring}}}&nbsp;°|No}}}}}}</includeonly><noinclude>{{Infobox/Part/JetEngine
+
<noinclude>}}
|name=Basic Jet Engine
 
|file=Basicjetengine.png
 
|costs=950
 
|mass=1
 
|drag=0.2
 
|temp=3600
 
|tolerance=7
 
|manufacturer=
 
|thrust=100
 
|stall=20
 
|opt-air=200
 
|in-size=1.1
 
|in-pow=125
 
|fuel=0.3
 
|vectoring=2.5
 
|since=v0.15
 
|part=JetEngine
 
}}
 
  
{{Tl|Infobox/Part}} implementation for jet engines.
+
{{Tl|Infobox/Part}} modules for [[jet engine]]s.
  
{{Infobox/Part/Sub|additional=
+
{{Parameter Table|name=text|parameters=
{{Parameter Row|thrust|Maximum Thrust}}
+
{{Parameter Row|thrust|Maximum thrust in kN}}
{{Parameter Row|stall|Stall Threshold}}
+
{{Parameter Row|stall|Stall threshold thrust in kN}}
{{Parameter Row|opt-air|Optimal Airflow}}
+
{{Parameter Row|isp|Specific impulse}}
{{Parameter Row|in-size|Intake air size}}
+
{{Parameter Row|vectoring|Thrust vectoring, if not set displays “No”.|Not set/No}}}}
{{Parameter Row|in-pow|Intake power}}
+
{{Subcategory|subtemplates}}</noinclude>
{{Parameter Row|fuel|Fuel Consumption}}
 
{{Parameter Row|vectoring|Thrust Vectoring|Not set/No}}}}</noinclude>
 

Revision as of 20:14, 28 December 2013

Maximum thrust 100 kN
Stall Threshold 10 kN
Isp 2000 s

Template:Infobox/Part/FuelConsumption Template:Infobox/Part/FuelConsumption

Thrust vectoring 2.5 °

{{Infobox/Part}} modules for jet engines.

Template:Parameter Table