This HTML5 document contains 41 embedded RDF statements represented using HTML+Microdata notation.

The embedded RDF content will be recognized by any processor of HTML5 Microdata.

Namespace Prefixes

PrefixIRI
dctermshttp://purl.org/dc/terms/
dbohttp://dbpedia.org/ontology/
foafhttp://xmlns.com/foaf/0.1/
n5https://global.dbpedia.org/id/
dbthttp://dbpedia.org/resource/Template:
rdfshttp://www.w3.org/2000/01/rdf-schema#
rdfhttp://www.w3.org/1999/02/22-rdf-syntax-ns#
owlhttp://www.w3.org/2002/07/owl#
wikipedia-enhttp://en.wikipedia.org/wiki/
dbphttp://dbpedia.org/property/
provhttp://www.w3.org/ns/prov#
dbchttp://dbpedia.org/resource/Category:
xsdhhttp://www.w3.org/2001/XMLSchema#
wikidatahttp://www.wikidata.org/entity/
dbrhttp://dbpedia.org/resource/

Statements

Subject Item
dbr:Met
dbo:wikiPageWikiLink
dbr:Microwave_electrothermal_thruster
dbo:wikiPageDisambiguates
dbr:Microwave_electrothermal_thruster
Subject Item
dbr:Microwave_electrothermal_thruster
rdfs:label
Microwave electrothermal thruster
rdfs:comment
Microwave electrothermal thruster, also known as MET, is a propulsion device that converts microwave energy (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.
dcterms:subject
dbc:Ion_engines
dbo:wikiPageID
65635767
dbo:wikiPageRevisionID
1059286241
dbo:wikiPageWikiLink
dbr:Arcjet_rocket dbr:Plasma_(physics) dbr:Propellant dbr:Electric_field dbr:Ion_thruster dbr:Electrically_powered_spacecraft_propulsion dbr:Conservation_of_momentum dbr:Spacecraft_propulsion dbr:Inelastic_collision dbr:Thrust dbr:Orbit_raising dbr:Specific_impulse dbr:Atmospheric_pressure dbr:Orbital_station-keeping dbr:Magnetron dbr:Resistojet_rocket dbr:Microwave dbr:Kinetic_energy dbc:Ion_engines
owl:sameAs
n5:FUpVw wikidata:Q104865033
dbp:wikiPageUsesTemplate
dbt:Spacecraft_propulsion dbt:Space-stub dbt:Reflist
dbo:abstract
Microwave electrothermal thruster, also known as MET, is a propulsion device that converts microwave energy (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.
prov:wasDerivedFrom
wikipedia-en:Microwave_electrothermal_thruster?oldid=1059286241&ns=0
dbo:wikiPageLength
9421
foaf:isPrimaryTopicOf
wikipedia-en:Microwave_electrothermal_thruster
Subject Item
dbr:Vigoride
dbo:wikiPageWikiLink
dbr:Microwave_electrothermal_thruster
Subject Item
dbr:Space_manufacturing
dbo:wikiPageWikiLink
dbr:Microwave_electrothermal_thruster
Subject Item
dbr:Ion_thruster
dbo:wikiPageWikiLink
dbr:Microwave_electrothermal_thruster
dbp:header
dbr:Microwave_electrothermal_thruster
Subject Item
dbr:Solar_electric_propulsion
dbo:wikiPageWikiLink
dbr:Microwave_electrothermal_thruster
Subject Item
wikipedia-en:Microwave_electrothermal_thruster
foaf:primaryTopic
dbr:Microwave_electrothermal_thruster