Difference between revisions of "Template:Infobox/Part/reaction engine"
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< Template:Infobox | Part
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| − | <noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Part/Thrust|{{{thrust<noinclude>|175</noinclude>}}}|{{{isp-atm<noinclude>|388</noinclude>}}}|{{{isp-vac|<noinclude>390</noinclude>}}}}} | + | <noinclude>{{Infobox/Part/preview| |
| + | </noinclude>{{Infobox/Part/Thrust|{{{thrust<noinclude>|175</noinclude>}}}|{{{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/ISP|{{{isp-atm<noinclude>|388</noinclude>}}}|{{{isp-vac|<noinclude>390</noinclude>}}}}} | ||
| − | {{Infobox/Part/consumption|{{#switch: {{{fuel|lfox}}} |x=100|sf=7500|mp=4000|lfox|#default=5000}}|{{{thrust<noinclude>|175</noinclude>}}}|{{#if: {{{isp-vac|<noinclude>390</noinclude>}}}|{{{isp-vac<noinclude>|390</noinclude>}}}|{{{isp-atm | + | {{Infobox/Part/consumption|{{#switch: {{{fuel|lfox}}} |x=100|sf=7500|mp=4000|lfox|#default=5000}}|{{{thrust<noinclude>|175</noinclude>}}}|{{#if: {{{isp-vac|<noinclude>390</noinclude>}}}|{{{isp-vac<noinclude>|390</noinclude>}}}|{{{isp-atm<noinclude>|388</noinclude>}}}}}|{{#switch: {{{fuel|lfox}}} |x={{mark|lgu}}|sf|mp|lfox|#default={{mark|fuelu}}}}|{{#switch: {{{fuel|lfox}}} |x=3|sf|mp|lfox|#default=2}}}} |
| − | {{Infobox/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|}}}|{{{vectoring}}} °|{{No}}}}}}<noinclude>}} | + | {{Infobox/Part/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 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: | ||
Latest revision as of 21:48, 10 September 2024
| Maximum thrust | (1 atm) | 174.10 kN |
| (vacuum) | 175.00 kN | |
| Isp | (1 atm) | 388 s |
| (vacuum) | 390 s | |
| Fuel consumption | 9.15  /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/Thrust}}, {{Infobox/Part/ISP}} and {{Infobox/Part/consumption}} to calculate the thrust based on Isp and thrust at atmospheric pressure. 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}}
| 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 Isp |
| vectoring | Yes | Thrust vectoring, if not set displays “No”. | Not set/No |
| fuel | Yes | Type of fuel. Supported:
|
lfox |
