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

From Kerbal Space Program Wiki
Jump to: navigation, search
(*use fuel parameter to determine density, unit and precession; *ion engines use separate template; !defaults to empty for Isp in vacuum;)
m (mismatched brackets)
 
(11 intermediate revisions by 5 users not shown)
Line 1: Line 1:
<noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust<noinclude>|175</noinclude>}}}&nbsp;kN}}
+
<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>}}}}}
 
{{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/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. 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/Thrust}}, {{Tl|Infobox/Part/ISP}} and {{Tl|Infobox/Part/consumption}} to calculate the thrust based on I<sub>sp</sub> and thrust at atmospheric pressure. 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)
 
* [[Jet engine]]s: {{Tl|Infobox/Part/jet engine}}
 
* [[Jet engine]]s: {{Tl|Infobox/Part/jet engine}}
  
{{Parameter Table|name=text|parameters=
+
{{Parameter table|name=text|parameters=
{{Parameter Row|thrust|Maximum thrust in kN}}
+
{{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)}}
+
{{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>}}
+
{{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|fuel|Type of fuel. Supported:
+
{{Parameter row|fuel|Type of fuel. Supported:
 
* '''<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>

Latest revision as of 01:09, 12 July 2021

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}}, {{Infobox/Part/ISP}} and {{Infobox/Part/consumption}} 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