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

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(Created page with "<noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust<noinclude>|175</noinclude>}}} kN}} {{Infobox/Part/ISP|{{{isp-a...")
 
(*use fuel parameter to determine density, unit and precession; *ion engines use separate template; !defaults to empty for Isp in vacuum;)
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<noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust<noinclude>|175</noinclude>}}}&nbsp;kN}}
 
<noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust<noinclude>|175</noinclude>}}}&nbsp;kN}}
{{Infobox/Part/ISP|{{{isp-atm<noinclude>|388</noinclude>}}}|{{{isp-vac<noinclude>|390</noinclude>}}}}}
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{{Infobox/Part/ISP|{{{isp-atm<noinclude>|388</noinclude>}}}|{{{isp-vac|<noinclude>390</noinclude>}}}}}
{{Infobox/Part/FuelConsumption|5000|{{{thrust<noinclude>|175</noinclude>}}}|{{{isp-atm<noinclude>|100</noinclude>}}}|{{{isp-vac<noinclude>|100</noinclude>}}}|{{{unit|l}}}|{{{consumption places|2}}}}}
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{{Infobox/Part/FuelConsumption|{{#switch: {{{fuel|lfox}}} |x=100|sf=7500|lfox|#default=5000}}|{{{thrust<noinclude>|175</noinclude>}}}|{{{isp-atm<noinclude>|388</noinclude>}}}|{{{isp-vac|<noinclude>390</noinclude>}}}|{{#switch: {{{fuel|lfox}}} |x=x|sf|lfox|#default=l}}|{{#switch: {{{fuel|lfox}}} |x=3|sf|lfox|#default=2}}}}
 
{{Infobox/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|}}}|{{{vectoring}}}&nbsp;°|{{No}}}}}}<noinclude>}}
 
{{Infobox/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|}}}|{{{vectoring}}}&nbsp;°|{{No}}}}}}<noinclude>}}
  
{{Tl|Infobox/Part}} modules for [[reaction engine]]s. Use this module directly for [[liquid fuel engine]]s and [[ion engine]]s. For [[solid rocket booster]]s the {{Tl|Infobox/Part/solid fuel engine}} should be used. It uses {{Tl|Infobox/Part/FuelConsumption}} to calculate the fuel consumption based on I<sub>sp</sub> and thrust.
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{{Tl|Infobox/Part}} modules for [[reaction engine]]s. Use this module directly for [[liquid fuel engine]]s. It uses {{Tl|Infobox/Part/FuelConsumption}} to calculate the fuel consumption based on I<sub>sp</sub> and thrust. Other engine types:
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* [[Solid rocket booster]]s: {{Tl|Infobox/Part/solid fuel engine}} (uses this template)
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* [[Ion engine]]s: {{Tl|Infobox/Part/ion engine}} (uses this template)
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* [[Jet engine]]s: {{Tl|Infobox/Part/jet engine}}
  
 
{{Parameter Table|name=text|parameters=
 
{{Parameter Table|name=text|parameters=
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{{Parameter Row|isp-vac|Specific impulse in vacuum.|Atmospheric I<sub>sp</sub>}}
 
{{Parameter Row|isp-vac|Specific impulse in vacuum.|Atmospheric I<sub>sp</sub>}}
 
{{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}}
{{Parameter Row|unit|Unit of the fuel consumed. Usually liters, but <tt>x</tt> for ion engines.|<tt>l</tt>}}
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{{Parameter Row|fuel|Type of fuel. Supported:
{{Parameter Row|consumption places|Number of decimal places used <nowiki>{{Infobox/Part/FuelConsumption}}</nowiki>.|2}}}}
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* '''<tt>lfox</tt>''' (default): Liquid fuel and oxidizer
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* '''<tt>sf</tt>''': Solid fuel
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* '''<tt>x</tt>''': Xenon gas|<tt>lfox</tt>}}}}
 
{{Subcategory|modules}}</noinclude>
 
{{Subcategory|modules}}</noinclude>

Revision as of 16:40, 10 February 2014

Maximum thrust 175 kN
Isp (1 atm) 388 s
(vacuum) 390 s
Fuel consumption (1 atm) 9.20 l/s
(vacuum) 9.15 l/s
Thrust vectoring No

{{Infobox/Part}} modules for reaction engines. Use this module directly for liquid fuel engines. It uses {{Infobox/Part/FuelConsumption}} to calculate the fuel consumption based on Isp and thrust. Other engine types:

Template:Parameter Table