Spacecraft Propulsion Devices and Systems with Microwave Excitation
In a spacecraft for operating a thruster that includes a microwave source, a resonant cavity, and a source of propellant which the thruster converts to hot gas and directs via a nozzle to generate thrust, a method includes operating the thruster in an ignition mode in which the microwave source outputs power at a first rate, and operating the thruster in a propulsion mode in which the microwave source outputs power at a second rate higher than the first rate.
1 . A method in a spacecraft for operating a thruster that includes a microwave source, a resonant cavity, and a source of propellant which the thruster converts to hot gas and directs via a nozzle to generate thrust, the method comprising:
operating the thruster in an ignition mode in which the microwave source outputs power at a first rate; and
operating the thruster in a propulsion mode in which the microwave source outputs power at a second rate higher than the first rate.