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...")
 
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<noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust<noinclude>|175</noinclude>}}}&nbsp;kN}}
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<noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Part/Thrust|{{{thrust<noinclude>|175</noinclude>}}}|{{{isp-atm<noinclude>|388</noinclude>}}}|{{{isp-vac|<noinclude>390</noinclude>}}}}}
{{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/consumption|{{#switch: {{{fuel|lfox}}} |x=100|sf=7500|mp=4000|lfox|#default=5000}}|{{{thrust<noinclude>|175</noinclude>}}}|{{#if: {{{isp-vac|<noinclude>390</noinclude>}}}|{{{isp-vac<noinclude>|390</noinclude>}}}|{{{isp-atm|<noinclude>388</noinclude>}}}}}|{{#switch: {{{fuel|lfox}}} |x={{mark|lgu}}|sf|mp|lfox|#default={{mark|fuelu}}}}|{{#switch: {{{fuel|lfox}}} |x=3|sf|mp|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 and [[RCS]] thrusters. It uses {{Tl|Infobox/Part/Thrust}} to calculate the thrust based on I<sub>sp</sub> and thrust at atmospheric pressure. 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=
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{{Parameter table|name=text|parameters=
{{Parameter Row|thrust|Maximum thrust in kN}}
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{{Parameter row|thrust|Vacuum thrust in kN (the value given in the part configuration)}}
{{Parameter Row|isp-atm|Specific impulse at Kerbin's sea level (1 atm)}}
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{{Parameter row|isp-atm|Specific impulse at Kerbin's sea level (1 atm)}}
{{Parameter Row|isp-vac|Specific impulse in vacuum.|Atmospheric I<sub>sp</sub>}}
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{{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}}
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{{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
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* '''<tt>mp</tt>''': Monopropellant|<tt>lfox</tt>}}}}
 
{{Subcategory|modules}}</noinclude>
 
{{Subcategory|modules}}</noinclude>

Revision as of 14:30, 14 April 2018

Maximum thrust (1 atm) 174.10 kN
(vacuum) 175.00 kN
Isp (1 atm) 388 s
(vacuum) 390 s
Fuel consumption 9.15 Units of fuel/s


Thrust vectoring No

{{Infobox/Part}} modules for reaction engines. Use this module directly for liquid fuel engines and RCS thrusters. It uses {{Infobox/Part/Thrust}} to calculate the thrust based on Isp and thrust at atmospheric pressure. Other engine types:

Name Optional Description Default
thrust No Vacuum thrust in kN (the value given in the part configuration)
isp-atm No Specific impulse at Kerbin's sea level (1 atm)
isp-vac Yes Specific impulse in vacuum. Atmospheric Isp
vectoring Yes Thrust vectoring, if not set displays “No”. Not set/No
fuel Yes Type of fuel. Supported:
  • lfox (default): Liquid fuel and oxidizer
  • sf: Solid fuel
  • x: Xenon gas
  • mp: Monopropellant
lfox