Difference between revisions of "Template:Infobox/Part/reaction engine"
From Kerbal Space Program Wiki
< Template:Infobox | Part
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 | + | {{Parameter row|thrust|Maximum thrust in kN}} |
| − | {{Parameter | + | {{Parameter row|isp-atm|Specific impulse at Kerbin's sea level (1 atm)}} |
| − | {{Parameter | + | {{Parameter row|isp-vac|Specific impulse in vacuum.|Atmospheric I<sub>sp</sub>}} |
| − | {{Parameter | + | {{Parameter row|vectoring|Thrust vectoring, if not set displays “No”.|Not set/No}} |
| − | {{Parameter | + | {{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 | |
| 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:
- Solid rocket boosters: {{Infobox/Part/solid fuel engine}} (uses this template)
- Ion engines: {{Infobox/Part/ion engine}} (uses this template)
- Jet engines: {{Infobox/Part/jet engine}}
