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

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m (*replace 'Parameter Row' and 'ParameterRow' by 'Parameter row';)
m (*renamed Parameter Table to Parameter table;)
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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=
+
{{Parameter table|name=text|parameters=
 
{{Parameter row|thrust|Maximum thrust in kN}}
 
{{Parameter row|thrust|Maximum thrust in kN}}
 
{{Parameter row|isp-atm|Specific impulse in seconds at Kerbin's sea level (1 atm)}}
 
{{Parameter row|isp-atm|Specific impulse in seconds at Kerbin's sea level (1 atm)}}

Revision as of 12:10, 19 December 2014

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
Fuel 433 Units of fuel
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
fuel No Solid fuel in this part in liters