Template:Infobox/Part/solid fuel engine

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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
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. Default: Atmospheric Isp
fuel × No Solid fuel in this part in liters