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- Q1423761 subject Q8784914.
- Q1423761 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.".
- Q1423761 wikiPageExternalLink www.irs.uni-stuttgart.de.
- Q1423761 wikiPageExternalLink lichtbogentriebwerk.html.
- Q1423761 wikiPageExternalLink electric-propulsion.
- Q1423761 wikiPageWikiLink Q122453.
- Q1423761 wikiPageWikiLink Q15818248.
- Q1423761 wikiPageWikiLink Q16787347.
- Q1423761 wikiPageWikiLink Q183.
- Q1423761 wikiPageWikiLink Q25236.
- Q1423761 wikiPageWikiLink Q4087.
- Q1423761 wikiPageWikiLink Q533668.
- Q1423761 wikiPageWikiLink Q556.
- Q1423761 wikiPageWikiLink Q58447.
- Q1423761 wikiPageWikiLink Q648588.
- Q1423761 wikiPageWikiLink Q8784914.
- Q1423761 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.".
- Q1423761 label "Arcjet rocket".