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- Arcjet_rocket abstract "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 of propellant (typically hydrazine or ammonia). This imparts additional energy to the propellant, so that one can extract more work out of each kilogram of propellant, at the expense of increased power consumption and (usually) higher cost. Also, the thrust levels available from typically used arcjet engines are very low compared with chemical engines.When the energy is available, arcjets are well suited to keeping stations in orbit and can replace monopropellant rockets.Aerojet MR-510 series arcjet engines are currently used on Lockheed Martin A2100 satellites using hydrazine as a propellant, providing over 585s average specific impulse at 2 kW.In Germany, researchers at the University of Stuttgart's Institute of Space Aviation Systems have been looking into these challenges for years and have developed various hydrogen-powered arcjet engines capable of power outputs from 1 to 100 kW. The heated hydrogen reaches exit speeds of 16 kilometres per second (9.9 mi/s). An arcjet-propelled test satellite by the name of Baden-Württemberg 1 (BW1) is scheduled to go to the Moon. Baden-Württemberg 1 would use polytetrafluoroethylene PTFE propellant.".
- Arcjet_rocket wikiPageExternalLink www.irs.uni-stuttgart.de.
- Arcjet_rocket wikiPageExternalLink lichtbogentriebwerk.html.
- Arcjet_rocket wikiPageExternalLink electric-propulsion.
- Arcjet_rocket wikiPageID "37836".
- Arcjet_rocket wikiPageLength "3272".
- Arcjet_rocket wikiPageOutDegree "12".
- Arcjet_rocket wikiPageRevisionID "707298963".
- Arcjet_rocket wikiPageWikiLink Ammonia.
- Arcjet_rocket wikiPageWikiLink Baden-Württemberg_1.
- Arcjet_rocket wikiPageWikiLink Category:Spacecraft_propulsion.
- Arcjet_rocket wikiPageWikiLink Electrically_powered_spacecraft_propulsion.
- Arcjet_rocket wikiPageWikiLink Germany.
- Arcjet_rocket wikiPageWikiLink Hydrazine.
- Arcjet_rocket wikiPageWikiLink Hydrogen.
- Arcjet_rocket wikiPageWikiLink MR-510.
- Arcjet_rocket wikiPageWikiLink Monopropellant_rocket.
- Arcjet_rocket wikiPageWikiLink Thrust.
- Arcjet_rocket wikiPageWikiLink University_of_Stuttgart.
- Arcjet_rocket wikiPageWikiLink Watt.
- Arcjet_rocket wikiPageWikiLinkText "Arcjet rocket".
- Arcjet_rocket wikiPageWikiLinkText "Arcjet".
- Arcjet_rocket wikiPageWikiLinkText "DC arcjet".
- Arcjet_rocket wikiPageWikiLinkText "arcjet rocket".
- Arcjet_rocket wikiPageWikiLinkText "arcjet".
- Arcjet_rocket wikiPageWikiLinkText "microwave arcjet".
- Arcjet_rocket wikiPageUsesTemplate Template:Convert.
- Arcjet_rocket wikiPageUsesTemplate Template:Reflist.
- Arcjet_rocket wikiPageUsesTemplate Template:Spacecraft_propulsion.
- Arcjet_rocket subject Category:Spacecraft_propulsion.
- Arcjet_rocket hypernym Form.
- Arcjet_rocket type Astrodynamic.
- Arcjet_rocket type Technology.
- Arcjet_rocket comment "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 of propellant (typically hydrazine or ammonia). This imparts additional energy to the propellant, so that one can extract more work out of each kilogram of propellant, at the expense of increased power consumption and (usually) higher cost.".
- Arcjet_rocket label "Arcjet rocket".
- Arcjet_rocket sameAs Q1423761.
- Arcjet_rocket sameAs Thermisches_Lichtbogentriebwerk.
- Arcjet_rocket sameAs Cohete_arcjet.
- Arcjet_rocket sameAs Arcjet.
- Arcjet_rocket sameAs DCアークジェット.
- Arcjet_rocket sameAs Arcjet_rocket.
- Arcjet_rocket sameAs m.09flp.
- Arcjet_rocket sameAs Электрический_ракетный_двигатель_термический.
- Arcjet_rocket sameAs Q1423761.
- Arcjet_rocket wasDerivedFrom Arcjet_rocket?oldid=707298963.
- Arcjet_rocket isPrimaryTopicOf Arcjet_rocket.