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

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(*use fuel parameter to determine density, unit and precession; *ion engines use separate template; !defaults to empty for Isp in vacuum;)
m (+mp fuel type support;)
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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>}}}}}
 
{{Infobox/Part/ISP|{{{isp-atm<noinclude>|388</noinclude>}}}|{{{isp-vac|<noinclude>390</noinclude>}}}}}
{{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/Part/FuelConsumption|{{#switch: {{{fuel|lfox}}} |x=100|sf=7500|mp=4000|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. It uses {{Tl|Infobox/Part/FuelConsumption}} to calculate the fuel consumption based on I<sub>sp</sub> and thrust. Other engine types:
+
{{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/FuelConsumption}} to calculate the fuel consumption based on I<sub>sp</sub> and thrust. Other engine types:
 
* [[Solid rocket booster]]s: {{Tl|Infobox/Part/solid fuel engine}} (uses this template)
 
* [[Solid rocket booster]]s: {{Tl|Infobox/Part/solid fuel engine}} (uses this template)
 
* [[Ion engine]]s: {{Tl|Infobox/Part/ion engine}} (uses this template)
 
* [[Ion engine]]s: {{Tl|Infobox/Part/ion engine}} (uses this template)
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* '''<tt>lfox</tt>''' (default): Liquid fuel and oxidizer
 
* '''<tt>lfox</tt>''' (default): Liquid fuel and oxidizer
 
* '''<tt>sf</tt>''': Solid fuel
 
* '''<tt>sf</tt>''': Solid fuel
* '''<tt>x</tt>''': Xenon gas|<tt>lfox</tt>}}}}
+
* '''<tt>x</tt>''': Xenon gas
 +
* '''<tt>mp</tt>''': Monopropellant|<tt>lfox</tt>}}}}
 
{{Subcategory|modules}}</noinclude>
 
{{Subcategory|modules}}</noinclude>

Revision as of 01:46, 11 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 and RCS thrusters. It uses {{Infobox/Part/FuelConsumption}} to calculate the fuel consumption based on Isp and thrust. Other engine types:

Template:Parameter Table