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Type of space propulsion using microwaves
Microwave electrothermal thruster, also known as MET, is a propulsion device that converts microwave energy (a type of electromagnetic radiation) into
Microwave electrothermal thruster
Microwave_electrothermal_thruster
American aerospace company
Orbital Service Vehicle (OSV), which utilizes proprietary Microwave Electrothermal Thrusters (MET) powered by water propellant. Originally focused on commercial
Momentus_space
Type of electric propulsion system
had previously developed the first commercially available microwave electrothermal thruster, for which the company received an order from ISRO. The ARKA-series
Hall-effect_thruster
Form of electric spacecraft propulsion
a team of engineers in developing a microwave electrothermal thruster (MET). In the discharge chamber, microwave (MW) energy flows into the center containing
Ion_thruster
Device claimed to be a propellantless spacecraft thruster
they had developed a valid electro-magnetic theory behind a microwave resonant cavity thruster. A demonstration version of the drive was built and tested
EmDrive
Type of spacecraft propulsion using electrical energy to accelerate propellant
thrusters, magnetoplasmadynamic thrusters, and pulsed inductive thrusters; and electrothermal devices such as resistojets and arcjets. Radio-frequency and
Spacecraft electric propulsion
Spacecraft_electric_propulsion
Space propulsion system
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
Gridded_ion_thruster
Spacecraft propulsion technology
demonstration in March 2018. An ABEP is composed by an intake and an electric thruster: rarefied gases which are responsible for drag in low Earth orbit (LEO)
Atmosphere-breathing electric propulsion
Atmosphere-breathing_electric_propulsion
Space propulsion system, a gridded electrostatic ion thruster
The NASA Evolutionary Xenon Thruster (NEXT) project at Glenn Research Center is a gridded electrostatic ion thruster about three times as powerful as the
NEXT_(ion_thruster)
Propulsion system creating motion without propellant
electrogravitics and lifters, gyroscopic and oscillation devices, microwave-cavity thrusters such as the EmDrive and Cannae drive, the helical engine, Mach-effect
Reactionless_drive
Type of rocket engine
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
Cold_gas_thruster
Type of electric propulsion
electron gun (hollow cathode). Such a thruster often generates the source plasma using radio frequency or microwave energy, using an external antenna. This
Plasma_propulsion_engine
Form of electrically powered spacecraft propulsion
Spacecraft propulsion – Method used to accelerate spacecraft VASIMR – Electrothermal thruster in developmentPages displaying short descriptions of redirect targets
Magnetoplasmadynamic_thruster
Proposed spacecraft propulsion method
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Bussard_ramjet
Type of propulsion for spacecraft
A pulsed plasma thruster (PPT) or as a plasma jet engine (PJE), is a form of electric spacecraft propulsion. PPTs are generally considered the simplest
Pulsed_plasma_thruster
Ion thruster subtype
A colloid thruster (or electrospray thruster) is a type of low thrust electric propulsion rocket engine that uses electrostatic acceleration of charged
Colloid_thruster
Type of rocket engine fuel
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
Hypergolic_propellant
Spacecraft propulsion device
arced across a solid propellant RF resonant cavity thruster, an electromagnetic thruster using microwaves Liquid apogee engine – A liquid-propellant rocket
Thrusters_(spacecraft)
Prototype spacecraft propulsion engine
The helicon double-layer thruster is a prototype electric spacecraft propulsion. It was created by Australian scientist Christine Charles, based on a technology
Helicon_double-layer_thruster
Electrothermal thruster in development
Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is an electrothermal thruster under development for possible use in spacecraft propulsion. It
Variable Specific Impulse Magnetoplasma Rocket
Variable_Specific_Impulse_Magnetoplasma_Rocket
Liquid form of rocket propellants
Anflo, K.; Moore, S.; King, P. Expanding the ADN-based Monopropellant Thruster Family. 23rd Annual AIAA/USU Conference on Small Satellites. SSC09-II-4
Liquid_rocket_propellant
perhaps 1.3 to 1.5 N (0.29 to 0.34 lbf), making them useful only for thrusters. In order to increase the power for medium-duration missions, engines
Radioisotope_rocket
The electrodeless plasma thruster is a spacecraft propulsion engine commercialized under the acronym "E-IMPAcT" for "Electrodeless-Ionization Magnetized
Electrodeless_plasma_thruster
Proposed nuclear pulse propulsion through antimatter-catalyzed nuclear chain reactions
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Antimatter-catalyzed nuclear pulse propulsion
Antimatter-catalyzed_nuclear_pulse_propulsion
Hypothetical spacecraft propulsion through continuous nuclear explosions for thrust
pulse propulsion Antimatter rocket Spacecraft electric propulsion Ion thruster Nuclear electric rocket Nuclear power in space Nuclear propulsion Nuclear
Nuclear_pulse_propulsion
Proposed spacelaunch method
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
Mass_driver
Physical and science fiction concept
Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer thruster Arcjet
Anti-gravity
Type of spacecraft propulsion system
reactor is converted to electrical energy, which is used to drive an ion thruster or other electrical spacecraft propulsion technology. The nuclear electric
Nuclear_electric_rocket
Propulsion concepts and technologies
and terrestrial field-matter coupling applications. Microwave electrothermal thrusters use microwave energy, potentially externally supplied, to heat a
Field_propulsion
Spacecraft propulsion system by NASA. 50kW Hall-effect thrusters, now for Lunar Gateway
electric power for its Hall-effect thrusters for maneuverability, which can be supported by chemical monopropellant thrusters for high-thrust attitude control
Advanced Electric Propulsion System
Advanced_Electric_Propulsion_System
Type of spacecraft electric propulsion system
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
Arcjet_rocket
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
Vacuum_arc_thruster
Proposed rocket propulsion mechanism
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Nuclear_salt-water_rocket
Space propulsion method using Sun radiation
solar sail has also been proposed to be addressed with a solar photon thruster. This also uses a reflective membrane, but unlike a conventional solar
Solar_sail
Type of spacecraft plasma propulsion system
A pulsed inductive thruster (PIT) is a form of ion thruster, used in spacecraft propulsion. It is a plasma propulsion engine using perpendicular electric
Pulsed_inductive_thruster
Conceptual rocket engine
expand through the magnetic nozzle and beyond, and thus, function as an ion thruster. The construction of the experimental research device and most of its early
Direct_Fusion_Drive
Rocket that burns 3 propellants at once or 2 fuels with an oxidizer, sequentially
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Tripropellant_rocket
Rocket that uses a single propellant with a catalyst
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
Monopropellant_rocket
Type of nuclear propulsion method with an ultra high specific-inpulse
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Fission-fragment_rocket
Mechanism where confined high-speed particles confer energy to a vehicle
either a microwave or a laser beam, and it is either pulsed or continuous. A continuous beam lends itself to thermal rockets, photonic thrusters, and light
Beam-powered_propulsion
Rocket with a motor that uses solid propellants
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Solid-propellant_rocket
Method of spacecraft propulsion
900 °C, specific impulse could be doubled in comparison to a cold gas thruster using the same propellant. In other words, a quadrupling of the temperature
Resistojet_rocket
Rocket driven by nuclear fusion power
fusion instead of direct thrust. Spacecraft propulsion methods such as ion thrusters require electric power to run but are highly efficient. In some cases
Fusion_rocket
Rocket engine operation method
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Expander_cycle
Rocket engine operation method
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Gas-generator_cycle
High efficiency engine for space travel
thruster High Power Electric Propulsion Pulsed plasma thruster Hall-effect thruster Magnetoplasmadynamic thruster Microwave electrothermal thruster Field-emission
Solar_electric_propulsion
Rocket engine operation method
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Staged_combustion_cycle
Space navigation technique
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Gravity_assist
Rocket engine operation method
Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer thruster Arcjet
Electric-pump-fed_engine
Type of rocket engine which uses liquid fuel stored at very low temperatures
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Cryogenic_rocket_engine
Rocket engine operation method
temperature fuel. Spacecraft attitude control and orbital maneuvering thrusters are almost universally pressure-fed designs. Examples include the Reaction
Pressure-fed_engine
Rocket engine power cycle
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Combustion_tap-off_cycle
Rocket engine that uses liquid fuels and oxidizers
orbital maneuvering system (OMS) engines and Reaction control system (RCS) thrusters. SpaceX's Draco and SuperDraco engines for the Dragon spacecraft. For
Liquid-propellant_rocket
Proposed spacecraft propulsion method
Magnetoplasmadynamic thruster (aka MPD Arc jet in Japan) in 2015, multiple antenna coils in 2019, and a multi-pole MPD thruster in 2020. Slough published
Magnetic_sail
Method used to accelerate spacecraft
Electrostatic ion thrusters Field-emission electric propulsion MagBeam thrusters Hall-effect thrusters Colloid thrusters Electrothermal thrusters, wherein electromagnetic
Spacecraft_propulsion
Rocket-propelled by exhausted coolant of a gas-cooled nuclear reactor
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Gas_core_reactor_rocket
Load bearing cable connecting objects in space
are currently tracked on radar and have predictable orbits. Although thrusters could be used to change the orbit of the system, a tether could also be
Space_tether
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Plasma_magnet
Nuclear spacecraft propulsion technology
long missions. Nuclear electric propulsion, by contrast, uses electric thrusters that can operate on dense, easily stored propellants such as xenon. In
Nuclear_thermal_rocket
Space propulsion system, electrostatic gridded ion thruster
Application Readiness (NSTAR) is a type of spacecraft ion thruster called electrostatic ion thruster. It is a highly efficient low-thrust spacecraft propulsion
NASA Solar Technology Application Readiness
NASA_Solar_Technology_Application_Readiness
Hypothetical type of spacecraft
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Nuclear_lightbulb
Launch system that only uses one rocket stage
than the potential energy that chemical fuel allows for, some laser or microwave powered rocket concepts have the potential to launch vehicles into orbit
Single-stage-to-orbit
Proposed spacecraft propulsion device
panels and reels to hold the wires; the main body, including chemical thrusters for adjusting trajectory en route and at destination and communications
Electric_sail
Rocket engine that uses photons to propel a spacecraft
to overcome the inherent inefficiency in producing thrust of the photon thruster by amplifying the momentum transfer of photons by recycling photons between
Nuclear_photonic_rocket
Rocket engine that uses both liquid / gaseous and solid fuel
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Hybrid-propellant_rocket
Type of nuclear thermal rocket
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Pulsed_nuclear_thermal_rocket
Hypothetical method of spacecraft propulsion
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Fission_sail
Type of solar sail
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Diffractive_solar_sail
with electric space propulsion. This includes both cruise engines and/or thrusters for altitude and orbit control. It is not specified whether the given
List of spacecraft with electric propulsion
List_of_spacecraft_with_electric_propulsion
Space tug by Momentus Space
depending on the exact customer specifications. Vigoride uses a microwave electrothermal thruster (MET) and water as the propellant. In 2019, the first test
Vigoride
Plasma Physics Experiment
Helicon double-layer thruster Arcjet rocket Resistojet rocket Microwave electrothermal thruster VASIMR Other Atmosphere-breathing electric propulsion High
Star_Thrust_Experiment
Topics referred to by the same term
toxic emissions Missing transverse energy in particle physics Microwave electrothermal thruster, a form of electric spacecraft propulsion The Metallurgical
Met
Theoretical spacecraft propulsion system
inbound to receive fuel from the depot. Solar-thermal monoprop hydrogen thrusters are also integral to the design of the next-generation cryogenic upper
Solar_thermal_rocket
Class of liquid rocket propellants
major classes of rocket fuels are: A common fuel in small maneuvering thrusters is hydrazine. It is liquid at room temperature and, having a positive
Nitrous_oxide_fuel_blend
US spacecraft
expected thrust force due to solar pressure is equivalent to 400 kW ion thruster systems used for comparable deep space missions. Spaceflight portal IKAROS
CubeSail_(UltraSail)
Type of electric spacecraft propulsion system
(FEEP) is an advanced electrostatic space propulsion concept, a form of ion thruster, that uses a liquid metal as a propellant – usually either caesium, indium
Field-emission electric propulsion
Field-emission_electric_propulsion
Chemical substance used for propulsion
using microwaves Radiofrequency ion thruster – generalization of HiPEP Hall-effect thruster, including its subtypes Stationary Plasma Thruster (SPT) and
Propellant
of the NIAC. MagBeam is different from a traditional electrostatic ion thruster in several ways, the primary one being that instead of the fuel and propulsion
MagBeam
in 2005. The HiPEP thruster differs from earlier ion thrusters because the xenon ions are produced using a combination of microwave and magnetic fields
High Power Electric Propulsion
High_Power_Electric_Propulsion
Production of manufactured goods in an environment outside a planetary atmosphere
sails, electric sails, magnetic sails, electric ion thrusters, microwave electrothermal thrusters, or mass drivers (this last method uses a sequence of
Space_manufacturing
Spacecraft propulsion using steam as propellant
the microwave-sized spacecraft extracted the water from hydrated artificial regolith and took off within the vacuum chamber using steam thrusters. The
World Is Not Enough (spacecraft propulsion)
World_Is_Not_Enough_(spacecraft_propulsion)
Monopropellant
hydrazine monopropellant for use in spacecraft's attitude control and thruster systems. It was derived from an earlier, similar formulation which came
Cavea-B
Soldier, engineer and inventor from the USA
exchangers. In the early 1990s, he conducted research on a Microwave Electrothermal Thruster, to which he developed a simple equilibrium based theory of
Scott_Haraburda
Vehicle propulsion using electromagnetic fields
in liquids. "Cold plasmas" with magnetic fields are subject to the electrothermal instability occurring at a critical Hall parameter, which makes full-scale
Magnetohydrodynamic_drive
Scott (June 1992). "Developmental Research for Designing a Microwave Electrothermal Thruster". 18th Army Science Conference. Vol. 2. Orlando, Florida.
List of people from Spencer, Indiana
List_of_people_from_Spencer,_Indiana
State of matter
with a high Hall parameter, a critical value triggers the problematic electrothermal instability which limited these technological developments.[citation
Plasma_(physics)
discharge Electrostatic ion cyclotron wave Electrostatic ion thruster Electrosurgery Electrothermal instability Electroweak epoch Elemental analysis Elliptic
List of plasma physics articles
List_of_plasma_physics_articles
Non-airbreathing engine used to propel a missile or vehicle
certain types of rocket engines can be extremely efficient (ex. hall effect thrusters). According to the writings of the Roman Aulus Gellius, the earliest known
Rocket_engine
Colorless flammable liquid with an ammonia-like odor
bulk-loaded liquid propellant gun programs for possible relevance to the electrothermal chemical propulsion program. The United States Air Force (USAF) regularly
Hydrazine
List of definitions of terms and concepts commonly used in aerospace engineering
Variable specific impulse magnetoplasma rocket – (VASIMR), is an electrothermal thruster under development for possible use in spacecraft propulsion. It
Glossary of aerospace engineering
Glossary_of_aerospace_engineering
New technologies actively in development
Laser Weapon System, Iron Beam Electrolaser Research and development Electrothermal-chemical technology Research and development Tank, artillery, and close-in
List_of_emerging_technologies
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MICROWAVE ELECTROTHERMAL-THRUSTER
MICROWAVE ELECTROTHERMAL-THRUSTER
MICROWAVE ELECTROTHERMAL-THRUSTER
MICROWAVE ELECTROTHERMAL-THRUSTER
MICROWAVE ELECTROTHERMAL-THRUSTER
MICROWAVE ELECTROTHERMAL-THRUSTER
MICROWAVE ELECTROTHERMAL-THRUSTER
MICROWAVE ELECTROTHERMAL-THRUSTER
MICROWAVE ELECTROTHERMAL-THRUSTER
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