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

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m (*replace 'Parameter Row' and 'ParameterRow' by 'Parameter row';)
m (*renamed Parameter Table to Parameter table;)
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* [[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|Maximum thrust in kN}}
 
{{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)}}

Revision as of 12:07, 19 December 2014

Maximum thrust 175 kN
Isp (1 atm) 388 s
(vacuum) 390 s

Template:Infobox/Part/FuelConsumption

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:

Name Optional Description Default
thrust No Maximum thrust in kN
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