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

Revision as of 01:09, 12 July 2021

{{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 I_sp 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 I_sp
`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`

@@ Line 4: / Line 4: @@
 {{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:
+{{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)
 * [[Ion engine]]s: {{Tl|Infobox/Part/ion engine}} (uses this template)