Microwave electrothermal thruster, also known as MET, is a propulsion device that converts microwave energy[1] (a type of electromagnetic radiation) into thermal (or heat) energy. These thrusters are predominantly used in spacecraft propulsion, more specifically to adjust the spacecraft’s position and orbit. A MET sustains and ignites a plasma in a propellant gas. This creates a heated propellant gas which in turn changes into thrust due to the expansion of the gas going through the nozzle. A MET’s heating feature is like one of an arc-jet (another propulsion device); however, due to the free-floating plasma, there are no problems with the erosion of metal electrodes, and therefore the MET is more efficient.[2]
^Bonnal, Christophe; DeLuca, Luigi T.; Haidn, Oskar J.; Frolov, Sergey M. (2009). Progress in Propulsion Physics Vol.1. EDP Sciences. pp. 425–438.
^US 10753346, Sherman, Daniel R.; Lukas, Edward & Quon, Brandon et al., "Control system for a microwave electrothermal thruster", published 2020-08-25, assigned to Northrop Grumman Systems Corp.
and 24 Related for: Microwave electrothermal thruster information
Microwaveelectrothermalthruster, also known as MET, is a propulsion device that converts microwave energy (a type of electromagnetic radiation) into...
a team of engineers in developing a microwaveelectrothermalthruster (MET). In the discharge chamber, microwave (MW) energy flows into the center containing...
"linear oscillating mechanism" reactionless drive; the gyroscopic inertial thruster is perhaps the best known example of a "rotating mechanism" reactionless...
Performance of electrothermal systems in terms of specific impulse (Isp) is 500 to ~1000 seconds, but exceeds that of cold gas thrusters, monopropellant...
the μ10, using microwaves, flew on the Hayabusa mission.[citation needed] In 2021, DART launched carrying a NEXT-C xenon ion thruster. In 2021, ThrustMe...
electron gun (hollow cathode). Such a thruster often generates the source plasma using radio frequency or microwave energy, using an external antenna. This...
A magnetoplasmadynamic (MPD) thruster (MPDT) is a form of electrically powered spacecraft propulsion which uses the Lorentz force (the force on a charged...
and reaction control thrusters: Apollo command and service module RCS, Space Shuttle OMS and RCS; Ariane 5 EPS; Draco thrusters used by the SpaceX Dragon...
is a concept for a thruster for spacecraft, first written about in 2001. It is purported to generate thrust by reflecting microwaves inside the device...
A pulsed plasma thruster (PPT), also known as a plasma jet engine, is a form of electric spacecraft propulsion. PPTs are generally considered the simplest...
A cold gas thruster (or a cold gas propulsion system) is a type of rocket engine which uses the expansion of a (typically inert) pressurized gas to generate...
storable propellant after passing it over a catalyst bed. The power for the thruster comes from the high pressure gas created during the decomposition reaction...
reach orbit. Well under a tenth of orbital velocity from a small rocket thruster is enough to raise perigee if a design prioritizes minimizing such, but...
An arcjet rocket or arcjet thruster is a form of electrically powered spacecraft propulsion, in which an electrical discharge (arc) is created in a flow...
pulse propulsion Antimatter rocket Spacecraft electric propulsion Ion thruster Nuclear electric rocket Nuclear power in space Nuclear propulsion Nuclear...
thruster High Power Electric Propulsion Pulsed plasma thruster Hall-effect thruster Magnetoplasmadynamic thrusterMicrowaveelectrothermalthruster Field-emission...
Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is an electrothermalthruster under development for possible use in spacecraft propulsion. It...
reactor is converted to electrical energy, which is used to drive an ion thruster or other electrical spacecraft propulsion technology. The nuclear electric...
electric power for its Hall-effect thrusters for maneuverability, which can be supported by chemical monopropellant thrusters for high-thrust attitude control...
Application Readiness (NSTAR) is a type of spacecraft ion thruster called electrostatic ion thruster. It is a highly efficient low-thrust spacecraft propulsion...
A vacuum arc thruster (VAT) is a form of electric spacecraft propulsion. It uses a vacuum arc discharge, across an insulator, between two electrodes to...
Combinator, and others. In 2019, Momentus claimed that its MicrowaveElectrothermalThruster (MET) was successfully tested in space, though the U.S. Securities...