First, Chemical Propulsion
Chemical propulsion is what most people think of when they hear “rocket engine”. Chemical rockets leverage chemical reactions (usually combustion of 2 rocket fuels) to release energy and generate thrust.
- Very high thrust
- Low specific impulse
- Operate in atmosphere or vacuum
Now, Electric Propulsion
Electric propulsion exhaust is made of charged particles, which feel and react to electric and magnetic fields. These fields accelerate the charged particles to high velocities to generate thrust.
- Relatively low thrust
- High specific impulse
- Operate in vacuum of space
Images courtesy of NASA.
What are “thrust” and “specific impulse”?
Thrust: The amount of force that an engine produces. With more thrust, you can increase your speed at a much faster rate and you can overcome much stronger opposing forces (such as gravity and atmospheric resistance).
Specific Impulse: A measure of the effectiveness of a rocket engine relative to the amount of propellant (fuel) it consumes. In some ways, specific impulse can be thought of as similar to the “miles per gallon” of a car. With higher specific impulse, the engine can do more with less fuel.
Specific impulse is measured in “seconds”. Chemical rockets cannot have specific impulse higher than about 500 seconds, limited by the amount of energy produced by the chemical reactions. Electric propulsion is only limited by the amount of electric power you can generate. While theoretically almost limitless, practical electric rockets have specific impulse as high as 5,000 seconds, up to 10 times higher than chemical propulsion!
If electric rockets are so efficient, why aren’t they used for everything?
The high efficiency of electric propulsion comes at the cost of a much lower thrust. Electric rockets do not generate enough thrust to launch a rocket from ground to orbit or to fight against the atmosphere. Additionally, even though electric rockets can do more with less propellant, the low thrust makes it so that it will take a longer time to do it. Electric propulsion is most useful for systems that are already in space and ones that value saving mass over a short misson duration.
Diverging Cusped Field (DCF) thruster test firing in SPL’s Astrovac test facility at MIT.