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

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m (Use part line)
m (Formatting)
 
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<noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Part/Thrust|{{{thrust<noinclude>|100</noinclude>}}}}}
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<noinclude>{{Infobox/Part/preview|
 +
</noinclude>{{Infobox/Part/Thrust|{{{thrust<noinclude>|100</noinclude>}}}}}
 
{{Infobox/Part/ISP|{{{isp<noinclude>|2000</noinclude>}}}|where=max}}
 
{{Infobox/Part/ISP|{{{isp<noinclude>|2000</noinclude>}}}|where=max}}
{{Infobox/Part/consumption|5000|{{{thrust<noinclude>|100</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}|{{mark|fuelu}}|2}}{{Infobox/Part/consumption|5000|{{{thrust<noinclude>|100</noinclude>}}}*{{{intake<noinclude>|22</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}|{{mark|airu}}|2|{{Infobox/Part/Dict|Consumption-air}}}}{{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>}}
+
{{Infobox/Part/consumption|5000|{{{thrust<noinclude>|100</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}|{{mark|fuelu}}|2}}
 +
{{Infobox/Part/consumption|5000|{{{thrust<noinclude>|100</noinclude>}}}*{{{intake<noinclude>|22</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}|{{mark|airu}}|2|{{Infobox/Part/Dict|Consumption-air}}}}
 +
{{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>
 +
}}
  
{{Tl|Infobox/Part}} modules for [[jet engine]]s. It uses {{Tl|Infobox/Part/ISP}} and {{Tl|Infobox/Part/FuelConsumption}}. Other engine types:
+
{{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:
 
* [[Liquid fuel engine]]s: {{Tl|Infobox/Part/reaction engine}}
 
* [[Liquid fuel engine]]s: {{Tl|Infobox/Part/reaction engine}}
 
* [[Solid rocket booster]]s: {{Tl|Infobox/Part/solid fuel engine}} (uses reaction engine template)
 
* [[Solid rocket booster]]s: {{Tl|Infobox/Part/solid fuel engine}} (uses reaction engine template)
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{{Parameter row|isp|The maximum specific impulse}}
 
{{Parameter row|isp|The maximum specific impulse}}
 
{{Parameter row|intake|The amount of IntakeAir is needed}}
 
{{Parameter row|intake|The amount of IntakeAir is needed}}
{{Parameter row|vectoring|Thrust vectoring, if not set displays “No”.|Not set/No}}}}
+
{{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