Difference between revisions of "Template:Infobox/Part/solid fuel engine"
From Kerbal Space Program Wiki
< Template:Infobox | Part
(Created page with "<noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Part/reaction engine|thrust={{{thrust<noinclude>|250</noinclude>}}}|isp-atm={{{isp-atm<noinclude>|225</noinclude>}}}|is...") |
m (Formattling and add vectoring as parameter) |
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− | <noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Part/reaction engine|thrust={{{thrust<noinclude>|250</noinclude>}}}|isp-atm={{{isp-atm<noinclude>|225</noinclude>}}}|isp-vac={{{isp-vac|<noinclude>240</noinclude>}}}| | + | <noinclude>{{Infobox/Part/preview| |
− | { | + | </noinclude>{{Infobox/Part/reaction engine|thrust={{{thrust<noinclude>|250</noinclude>}}}|isp-atm={{{isp-atm<noinclude>|225</noinclude>}}}|isp-vac={{{isp-vac|<noinclude>240</noinclude>}}}|vectoring={{{vectoring|}}}|fuel=sf}} |
− | {{Infobox/Part/Line|{{ | + | {{Infobox/Part/Line|{{Infobox/Part/Dict|Burn}}|{{#expr: {{{fuel<noinclude>|433</noinclude>}}}/{{FuelConsumption|{{{isp-atm<noinclude>|225</noinclude>}}}|{{{thrust<noinclude>|250</noinclude>}}}|7500}} round 1}} {{Dict|s}}|{{#if: {{{isp-vac|<noinclude>240</noinclude>}}}|{{#expr: {{{fuel<noinclude>|433</noinclude>}}}/{{FuelConsumption|{{{isp-vac<noinclude>|240</noinclude>}}}|{{{thrust<noinclude>|250</noinclude>}}}|7500}} round 1}} {{Dict|s}}}}}}<noinclude> |
+ | }} | ||
{{Tl|Infobox/Part}} modules for [[solid rocket booster]]s. It uses {{Tl|Infobox/Part/reaction engine}} and {{Tl|FuelConsumption}}. Other engine types: | {{Tl|Infobox/Part}} modules for [[solid rocket booster]]s. It uses {{Tl|Infobox/Part/reaction engine}} and {{Tl|FuelConsumption}}. Other engine types: | ||
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* [[Jet engine]]s: {{Tl|Infobox/Part/jet engine}} | * [[Jet engine]]s: {{Tl|Infobox/Part/jet engine}} | ||
− | {{Parameter | + | {{Parameter table|name=text|parameters= |
− | {{Parameter | + | {{Parameter row|thrust|Maximum thrust in kN}} |
− | {{Parameter | + | {{Parameter row|isp-atm|Specific impulse in seconds at Kerbin's sea level (1 atm)}} |
− | {{Parameter | + | {{Parameter row|isp-vac|Specific impulse in seconds in vacuum.|Atmospheric I<sub>sp</sub>}} |
− | {{Parameter | + | {{Parameter row|vectoring|Thrust vectoring, if not set displays “No”.|Not set/No}} |
+ | {{Parameter row|fuel|The amount of Solid fuel in this part in liters}} | ||
+ | }} | ||
{{Subcategory|modules}}</noinclude> | {{Subcategory|modules}}</noinclude> |
Latest revision as of 22:04, 10 September 2024
Maximum thrust | (1 atm) | 234.38 kN |
(vacuum) | 250.00 kN | |
Isp | (1 atm) | 225 s |
(vacuum) | 240 s | |
Fuel consumption | 14.16 /s | |
Thrust vectoring | No | |
Burn time | (1 atm) | 28.7 s |
(vacuum) | 30.6 s |
{{Infobox/Part}} modules for solid rocket boosters. It uses {{Infobox/Part/reaction engine}} and {{FuelConsumption}}. Other engine types:
- Liquid fuel engines: {{Infobox/Part/reaction engine}}
- Ion engines: {{Infobox/Part/ion engine}} (uses reaction engine template)
- Jet engines: {{Infobox/Part/jet engine}}
Name | Optional | Description | Default |
---|---|---|---|
thrust | No | Maximum thrust in kN | |
isp-atm | No | Specific impulse in seconds at Kerbin's sea level (1 atm) | |
isp-vac | Yes | Specific impulse in seconds in vacuum. | Atmospheric Isp |
vectoring | Yes | Thrust vectoring, if not set displays “No”. | Not set/No |
fuel | No | The amount of Solid fuel in this part in liters |