Difference between revisions of "Template:Infobox/Part/solid fuel engine"
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< 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...") |
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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}} | <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}} | ||
{{Infobox/Line|{{Infobox/Part/Dict|Fuel}}|{{{fuel<noinclude>|433</noinclude>}}} L}} | {{Infobox/Line|{{Infobox/Part/Dict|Fuel}}|{{{fuel<noinclude>|433</noinclude>}}} L}} | ||
− | {{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}} 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}} s}}}}<noinclude>}} | + | {{Infobox/Part/Line|{{lang|en=Burn time|de=Brenndauer|pl=Czas pracy|ja=燃焼時間}}|{{#expr: {{{fuel<noinclude>|433</noinclude>}}}/{{FuelConsumption|{{{isp-atm<noinclude>|225</noinclude>}}}|{{{thrust<noinclude>|250</noinclude>}}}|7500}} round 1}} 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}} 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: |
Revision as of 15:47, 24 September 2014
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 | |
Fuel | 433 L | |
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}}