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

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m (More info about which templates are used)
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{{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 [[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:
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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 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