Difference between revisions of "Template:Infobox/Part/jet engine"
From Kerbal Space Program Wiki
< Template:Infobox | Part
m (Move translations to dict) |
m (Use the same template as reaction engine) |
||
| Line 1: | Line 1: | ||
| − | <noinclude>{{Infobox/Part/preview|</noinclude> | + | <noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Part/Thrust|{{{thrust<noinclude>|100</noinclude>}}}}} |
{{Infobox/Part/ISP|{{{isp<noinclude>|2000</noinclude>}}}|where=max}} | {{Infobox/Part/ISP|{{{isp<noinclude>|2000</noinclude>}}}|where=max}} | ||
| − | {{Infobox/Part/ | + | {{Infobox/Part/consumption|5000|{{{thrust<noinclude>|100</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}|{{mark|fuelu}}|2}}{{Infobox/Part/consumption|5000|{{{thrust<noinclude>|100</noinclude>}}}*{{{intake<noinclude>|22</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}|{{mark|airu}}|2|{{Infobox/Part/Dict|Consumption-air}}}}{{Infobox/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|<noinclude>2.5</noinclude>}}}|{{{vectoring<noinclude>|2.5</noinclude>}}} °|{{No}}}}}}<noinclude>}} |
| − | {{Infobox/Part/ | ||
| − | {{Infobox/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|<noinclude>2.5</noinclude>}}}|{{{vectoring<noinclude>|2.5</noinclude>}}} °|{{No}}}}}}<noinclude>}} | ||
{{Tl|Infobox/Part}} modules for [[jet engine]]s. It uses {{Tl|Infobox/Part/ISP}} and {{Tl|Infobox/Part/FuelConsumption}}. Other engine types: | {{Tl|Infobox/Part}} modules for [[jet engine]]s. It uses {{Tl|Infobox/Part/ISP}} and {{Tl|Infobox/Part/FuelConsumption}}. Other engine types: | ||
| Line 13: | Line 11: | ||
{{Parameter row|thrust|Maximum thrust in kN}} | {{Parameter row|thrust|Maximum thrust in kN}} | ||
{{Parameter row|isp|The maximum specific impulse}} | {{Parameter row|isp|The maximum specific impulse}} | ||
| + | {{Parameter row|intake|The amount of IntakeAir is needed}} | ||
{{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}}}} | ||
{{Subcategory|modules}}</noinclude> | {{Subcategory|modules}}</noinclude> | ||
Revision as of 22:53, 1 September 2024
| Maximum thrust | 100.00 kN | |||||||
| Isp | (max) | 2000 s | ||||||
| Fuel consumption | 1.02  /s|- valign="top"
|
Intake air consumption | 22.43  /s|- valign="top"
|
Thrust vectoring | 2.5 ° | |||
{{Infobox/Part}} modules for jet engines. It uses {{Infobox/Part/ISP}} and {{Infobox/Part/FuelConsumption}}. Other engine types:
- Liquid fuel engines: {{Infobox/Part/reaction engine}}
- Solid rocket boosters: {{Infobox/Part/solid fuel engine}} (uses reaction engine template)
- Ion engines: {{Infobox/Part/ion engine}} (uses reaction engine template)
| Name | Optional | Description | Default |
|---|---|---|---|
| thrust | No | Maximum thrust in kN | |
| isp | No | The maximum specific impulse | |
| intake | No | The amount of IntakeAir is needed | |
| vectoring | Yes | Thrust vectoring, if not set displays “No”. | Not set/No |
