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

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m (*replace 'Parameter Row' and 'ParameterRow' by 'Parameter row';)
m (Formatting)
 
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<noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust<noinclude>|100</noinclude>}}}&nbsp;kN}}
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<noinclude>{{Infobox/Part/preview|
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{{Infobox/Part/ISP|{{{isp<noinclude>|2000</noinclude>}}}}}
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</noinclude>{{Infobox/Part/Thrust|{{{thrust<noinclude>|100</noinclude>}}}}}
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{{Infobox/Part/FuelConsumption|5000|{{{thrust<noinclude>|100</noinclude>}}}/16|{{{isp<noinclude>|100</noinclude>}}}||{{mark|fuelu}}|2}}
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{{Infobox/Part/ISP|{{{isp<noinclude>|2000</noinclude>}}}|where=max}}
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{{Infobox/Part/FuelConsumption|5000|{{{thrust<noinclude>|100</noinclude>}}}/16*15|{{{isp<noinclude>|100</noinclude>}}}||{{mark|airu}}|2|{{lang|en=Intake air consumption|pl=Zużycie wlotu powietrza|hu=Levegő&shy;fogyasztás|ja=必要吸気量}}}}
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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|[[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/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/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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}}
  
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{{Tl|Infobox/Part}} modules for [[jet engine]]s.
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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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{{Parameter Table|name=text|parameters=
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{{Parameter table|name=text|parameters=
 
{{Parameter row|thrust|Maximum thrust in kN}}
 
{{Parameter row|thrust|Maximum thrust in kN}}
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{{Parameter row|isp|Specific impulse}}
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{{Parameter row|isp|The maximum specific impulse}}
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{{Parameter row|vectoring|Thrust vectoring, if not set displays “No”.|Not set/No}}}}
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{{Parameter row|intake|The amount of IntakeAir is needed}}
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{{Parameter row|vectoring|Thrust vectoring, if not set displays “No”.|Not set/No}}
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}}
 
{{Subcategory|modules}}</noinclude>
 
{{Subcategory|modules}}</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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