Difference between revisions of "Template:Infobox/Part/reaction engine"
From Kerbal Space Program Wiki
< Template:Infobox | Part
(*use variable thrust and fixed fuel flow;) |
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| Line 1: | Line 1: | ||
| − | <noinclude>{{Infobox/Part/preview|</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/ | + | {{Infobox/Part/consumption|{{#switch: {{{fuel|lfox}}} |x=100|sf=7500|mp=4000|lfox|#default=5000}}|{{{thrust<noinclude>|175</noinclude>}}}|{{{isp-atm<noinclude>|388</noinclude>}}}|{{#switch: {{{fuel|lfox}}} |x={{mark|lgu}}|sf|lfox|#default={{mark|fuelu}}}}|{{#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 and [[RCS]] thrusters. It uses {{Tl|Infobox/Part/ | + | {{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}} to calculate the thrust based on I<sub>sp</sub> and thrust at atmospheric pressure. 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) | ||
| Line 10: | Line 10: | ||
{{Parameter table|name=text|parameters= | {{Parameter table|name=text|parameters= | ||
| − | {{Parameter row|thrust| | + | {{Parameter row|thrust|Atmospheric thrust in kN (the value given in the part configuration)}} |
{{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>}} | ||
Revision as of 09:42, 1 May 2015
| Maximum thrust | (1 atm) | 174.10 kN |
| (vacuum) | 175.00 kN | |
| Isp | (1 atm) | 388 s |
| (vacuum) | 390 s | |
| Fuel consumption | 9.20  /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}} 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 | Atmospheric 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 |
