Difference between revisions of "Template:Infobox/Part/solid fuel engine"

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(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>}}}|fuel=sf}}
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<noinclude>{{Infobox/Part/preview|
{{Infobox/Line|{{Infobox/Part/Dict|Fuel}}|{{{fuel<noinclude>|433</noinclude>}}}&nbsp;L}}
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</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|{{lang|en=Burn time|de=Brenndauer|pl=Czas pracy}}|{{#expr: {{{fuel<noinclude>|433</noinclude>}}}/{{FuelConsumption|{{{isp-atm<noinclude>|225</noinclude>}}}|{{{thrust<noinclude>|250</noinclude>}}}|7500}} round 1}}&nbsp;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}}&nbsp;s}}}}<noinclude>}}
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{{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}}&nbsp;{{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}}&nbsp;{{Dict|s}}}}}}<noinclude>
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}}
  
 
{{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 Table|name=text|parameters=
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{{Parameter table|name=text|parameters=
{{Parameter Row|thrust|Maximum thrust in kN}}
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{{Parameter row|thrust|Maximum thrust in kN}}
{{Parameter Row|isp-atm|Specific impulse in seconds at Kerbin's sea level (1 atm)}}
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{{Parameter row|isp-atm|Specific impulse in seconds at Kerbin's sea level (1 atm)}}
{{Parameter Row|isp-vac|Specific impulse in seconds in vacuum.|Atmospheric I<sub>sp</sub>}}
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{{Parameter row|isp-vac|Specific impulse in seconds in vacuum.|Atmospheric I<sub>sp</sub>}}
{{Parameter Row|fuel|Solid fuel in this part in liters}}}}
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{{Parameter row|vectoring|Thrust vectoring, if not set displays “No”.|Not set/No}}
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{{Parameter row|fuel|The amount of Solid fuel in this part in liters}}
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}}
 
{{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 Units of fuel/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:

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