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

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m (*switched isp selection;)
m (Formatting)
 
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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>}}}}}
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<noinclude>{{Infobox/Part/preview|
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</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/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>|388</noinclude>}}}|{{{isp-atm|<noinclude>390</noinclude>}}}}}|{{#switch: {{{fuel|lfox}}} |x={{mark|lgu}}|sf|lfox|#default={{mark|fuelu}}}}|{{#switch: {{{fuel|lfox}}} |x=3|sf|lfox|#default=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>}}
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{{Infobox/Part/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|}}}|{{{vectoring}}}&nbsp;°|{{No}}}}}}<noinclude>
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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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{{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)

Latest revision as of 21:48, 10 September 2024

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