Difference between revisions of "Template:Infobox/Part/jet engine"
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< Template:Infobox | Part
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{{Infobox/Part/ISP|{{{isp<noinclude>|2000</noinclude>}}}|where=max}} | {{Infobox/Part/ISP|{{{isp<noinclude>|2000</noinclude>}}}|where=max}} | ||
{{Infobox/Part/FuelConsumption|5000|{{{thrust<noinclude>|100</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}||{{mark|fuelu}}|2}} | {{Infobox/Part/FuelConsumption|5000|{{{thrust<noinclude>|100</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}||{{mark|fuelu}}|2}} | ||
− | {{Infobox/Part/FuelConsumption|5000|{{{thrust<noinclude>|100</noinclude>}}}*{{{intake<noinclude>|22</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}||{{mark|airu}}|2|{{lang|en=Intake air consumption|pl=Zużycie wlotu powietrza|hu=Levegő­fogyasztás|ja=必要吸気量}}}} | + | {{Infobox/Part/FuelConsumption|5000|{{{thrust<noinclude>|100</noinclude>}}}*{{{intake<noinclude>|22</noinclude>}}}|{{{isp<noinclude>|2000</noinclude>}}}||{{mark|airu}}|2|{{lang|en=Intake air consumption|pl=Zużycie wlotu powietrza|hu=Levegő­fogyasztás|ja=必要吸気量|tr=Giren hava tüketimi}}}} |
{{Infobox/Line|[[Thrust vectoring{{if lang}}|{{Infobox/Part/Dict|Vectoring}}]]|{{#if: {{{vectoring|<noinclude>2.5</noinclude>}}}|{{{vectoring<noinclude>|2.5</noinclude>}}} °|{{No}}}}}}<noinclude>}} | {{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. | + | {{Tl|Infobox/Part}} modules for [[jet engine]]s. It uses {{Tl|Infobox/Part/ISP}} and {{Tl|Infobox/Part/FuelConsumption}}. Other engine types: |
+ | * [[Liquid fuel engine]]s: {{Tl|Infobox/Part/reaction engine}} | ||
+ | * [[Solid rocket booster]]s: {{Tl|Infobox/Part/solid fuel engine}} (uses reaction engine template) | ||
+ | * [[Ion engine]]s: {{Tl|Infobox/Part/ion engine}} (uses reaction engine template) | ||
{{Parameter table|name=text|parameters= | {{Parameter table|name=text|parameters= |
Latest revision as of 06:48, 10 July 2021
Maximum thrust | 100 kN | |
Isp | (max) | 2000 s |
Fuel consumption | 1.02 /s | |
Intake air consumption | 22.43 /s | |
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 | |
vectoring | Yes | Thrust vectoring, if not set displays “No”. | Not set/No |