liquid rocket
Propellant-burning spacecraft engine
A liquid rocket uses liquid propellants—typically a fuel and an oxidizer stored in separate tanks—that are pumped into a combustion chamber where they mix and ignite.
This distinguishes them from solid rockets, which use pre-mixed solid fuel.
Liquid rockets offer more control: thrust can be throttled, stopped, and restarted.
The Saturn V used liquid rocket engines to reach the moon.
Extremely low temperature
Machine producing motion
- nozzleFlow-directing pipe fitting
- combustion chamberEngine's ignition cavity
- turbopumpRotary propellant pressurizer
- injectorMechanism forcing substances inward
oxidizer · fuel · gimbal · gas generator · propellant · igniter · ablative · aerospike
Forceful forward motion
- burn timeHow long something flames
- restartableAble to begin anew
- delta-vSpacecraft maneuver measurement
- thrust-to-weightForce output divided by mass
cryogenic
Extremely low temperature
engine
Machine producing motion
- nozzleFlow-directing pipe fitting
- combustion chamberEngine's ignition cavity
- turbopumpRotary propellant pressurizer
injector · oxidizer · fuel · gimbal · gas generator · propellant · igniter · ablative · aerospike
thrust
Forceful forward motion
- burn timeHow long something flames
- restartableAble to begin anew
- delta-vSpacecraft maneuver measurement
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