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

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m (*use dict instead of lang;)
m (*replace 'Parameter Row' and 'ParameterRow' by 'Parameter row';)
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{{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)}}
{{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

Revision as of 20:54, 26 November 2014

Maximum thrust 175 kN
Isp (1 atm) 388 s
(vacuum) 390 s
Fuel consumption (1 atm) 9.20 l/s
(vacuum) 9.15 l/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/FuelConsumption}} to calculate the fuel consumption based on Isp and thrust. Other engine types:

Template:Parameter Table