Difference between revisions of "Template:Infobox/Part/reaction engine"
From Kerbal Space Program Wiki
< Template:Infobox | Part
(*use fuel parameter to determine density, unit and precession; *ion engines use separate template; !defaults to empty for Isp in vacuum;) |
m (+mp fuel type support;) |
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<noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust<noinclude>|175</noinclude>}}} kN}} | <noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust<noinclude>|175</noinclude>}}} kN}} | ||
{{Infobox/Part/ISP|{{{isp-atm<noinclude>|388</noinclude>}}}|{{{isp-vac|<noinclude>390</noinclude>}}}}} | {{Infobox/Part/ISP|{{{isp-atm<noinclude>|388</noinclude>}}}|{{{isp-vac|<noinclude>390</noinclude>}}}}} | ||
| − | {{Infobox/Part/FuelConsumption|{{#switch: {{{fuel|lfox}}} |x=100|sf=7500|lfox|#default=5000}}|{{{thrust<noinclude>|175</noinclude>}}}|{{{isp-atm<noinclude>|388</noinclude>}}}|{{{isp-vac|<noinclude>390</noinclude>}}}|{{#switch: {{{fuel|lfox}}} |x=x|sf|lfox|#default=l}}|{{#switch: {{{fuel|lfox}}} |x=3|sf|lfox|#default=2}}}} | + | {{Infobox/Part/FuelConsumption|{{#switch: {{{fuel|lfox}}} |x=100|sf=7500|mp=4000|lfox|#default=5000}}|{{{thrust<noinclude>|175</noinclude>}}}|{{{isp-atm<noinclude>|388</noinclude>}}}|{{{isp-vac|<noinclude>390</noinclude>}}}|{{#switch: {{{fuel|lfox}}} |x=x|sf|lfox|#default=l}}|{{#switch: {{{fuel|lfox}}} |x=3|sf|lfox|#default=2}}}} |
{{Infobox/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|}}}|{{{vectoring}}} °|{{No}}}}}}<noinclude>}} | {{Infobox/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|}}}|{{{vectoring}}} °|{{No}}}}}}<noinclude>}} | ||
| − | {{Tl|Infobox/Part}} modules for [[reaction engine]]s. Use this module directly for [[liquid fuel engine]]s. It uses {{Tl|Infobox/Part/FuelConsumption}} to calculate the fuel consumption based on I<sub>sp</sub> and thrust. 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/FuelConsumption}} to calculate the fuel consumption based on I<sub>sp</sub> and thrust. 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) | ||
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* '''<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 | ||
| − | * '''<tt>x</tt>''': Xenon gas|<tt>lfox</tt>}}}} | + | * '''<tt>x</tt>''': Xenon gas |
| + | * '''<tt>mp</tt>''': Monopropellant|<tt>lfox</tt>}}}} | ||
{{Subcategory|modules}}</noinclude> | {{Subcategory|modules}}</noinclude> | ||
Revision as of 01:46, 11 February 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}}
