#electricpropulsion — Public Fediverse posts
Live and recent posts from across the Fediverse tagged #electricpropulsion, aggregated by home.social.
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#SASIC:
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Neumann commissions propulsion tech on CarbSAR satellite
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"South Australian-based electric propulsion company Neumann Space has successfully commissioned its electric propulsion technology, the Neumann Drive® ND-50, completing the system’s demonstration phase in space and clearing the way for commercial deployment."https://sasic.sa.gov.au/news/neumann-commissions-propulsion-tech-on-carbsar-satellite/
19.5.2026
#CarbSAR #ElectricPropulsion #ElectricThruster #Ionentriebwerk #NeumannSpace #ND50 #Raumfahrt #SAR #Satelliten #SpaceFlight #SSTL
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#SASIC:
"
Neumann commissions propulsion tech on CarbSAR satellite
"
"South Australian-based electric propulsion company Neumann Space has successfully commissioned its electric propulsion technology, the Neumann Drive® ND-50, completing the system’s demonstration phase in space and clearing the way for commercial deployment."https://sasic.sa.gov.au/news/neumann-commissions-propulsion-tech-on-carbsar-satellite/
19.5.2026
#CarbSAR #ElectricPropulsion #ElectricThruster #Ionentriebwerk #NeumannSpace #ND50 #Raumfahrt #SAR #Satelliten #SpaceFlight #SSTL
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#ElectricPropulsion uses up to 90% less 📉 propellant than traditional, high-thrust chemical rockets. During tests, the #NASA JPL team achieved power levels of up to 120 kilowatts. That’s over 25 times 📈 the power of the thrusters on Psyche. The team aims to reach power levels between 500 kilowatts and 1 megawatt per thruster. A human 🧑🚀 mission to #Mars might need 2 to 4 megawatts of power, requiring multiple MPD thrusters https://www.jpl.nasa.gov/news/nasa-fires-up-powerful-lithium-fed-thruster-for-trips-to-mars/
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#ElectricPropulsion uses up to 90% less 📉 propellant than traditional, high-thrust chemical rockets. During tests, the #NASA JPL team achieved power levels of up to 120 kilowatts. That’s over 25 times 📈 the power of the thrusters on Psyche. The team aims to reach power levels between 500 kilowatts and 1 megawatt per thruster. A human 🧑🚀 mission to #Mars might need 2 to 4 megawatts of power, requiring multiple MPD thrusters https://www.jpl.nasa.gov/news/nasa-fires-up-powerful-lithium-fed-thruster-for-trips-to-mars/
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Rocket Lab’s Gauss Thruster Launch Adds New Angle To RKLB Story
Make better investment decisions with Simply Wall St’s easy, visual tools that give you a competitive edge. Rocket…
#NewsBeep #News #Space #AU #Australia #electricpropulsion #Gauss #RocketLab #satelliteoperators #Science #spacesystems
https://www.newsbeep.com/au/608447/ -
Rocket Lab’s Gauss Thruster Launch Adds New Angle To RKLB Story
Make better investment decisions with Simply Wall St’s easy, visual tools that give you a competitive edge. Rocket…
#NewsBeep #News #Space #AU #Australia #electricpropulsion #Gauss #RocketLab #satelliteoperators #Science #spacesystems
https://www.newsbeep.com/au/608447/ -
https://www.europesays.com/ie/436221/ Rocket Lab’s Gauss Thruster Launch Adds New Angle To RKLB Story #Éire #ElectricPropulsion #Gauss #IE #Ireland #RocketLab #SatelliteOperators #Science #Space #SpaceSystems
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#NASA will launch the #SpaceReactor1 Freedom, the first nuclear ☢️ powered #interplanetary spacecraft, to #Mars 🔴 before the end of 📆 2028. Nuclear #ElectricPropulsion enables high power missions beyond #Jupiter 🪐 where #solar arrays are not effective https://www.nasa.gov/news-release/nasa-unveils-initiatives-to-achieve-americas-national-space-policy/
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#NASA will launch the #SpaceReactor1 Freedom, the first nuclear ☢️ powered #interplanetary spacecraft, to #Mars 🔴 before the end of 📆 2028. Nuclear #ElectricPropulsion enables high power missions beyond #Jupiter 🪐 where #solar arrays are not effective https://www.nasa.gov/news-release/nasa-unveils-initiatives-to-achieve-americas-national-space-policy/
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#GeneralGalactic’s water 💧 propulsion system could provide 5-10 times the Delta-V of traditional systems. For #chemical propulsion, it will use electrolysis to split water, then burn the hydrogen with oxygen as the oxidizer. For #electrical propulsion, it will split water and then apply sufficient electrical energy 🔋 to convert the oxygen into plasma. It will then use a #magnetic field to guide the plasma out of a thruster https://interestingengineering.com/space/satellite-using-water-powered-propulsion-system
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#GeneralGalactic’s water 💧 propulsion system could provide 5-10 times the Delta-V of traditional systems. For #chemical propulsion, it will use electrolysis to split water, then burn the hydrogen with oxygen as the oxidizer. For #electrical propulsion, it will split water and then apply sufficient electrical energy 🔋 to convert the oxygen into plasma. It will then use a #magnetic field to guide the plasma out of a thruster https://interestingengineering.com/space/satellite-using-water-powered-propulsion-system
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⚓⚡ Smidmart | Precision Monitoring for Modern Marine Propulsion
In today’s electric-propulsion vessels digital voltmeters and ammeters play a central role in that reliability.
Smidmart -https://zurl.co/kyMu8
#Smidmart #MarineEngineering #ElectricPropulsion #ShipSystems -
In an #electrospray thruster, charged particles are pulled directly out of a liquid propellant using a strong electric field and accelerated using charged #electrodes https://spacepropulsion.mit.edu/electric-propulsion
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In an #electrospray thruster, charged particles are pulled directly out of a liquid propellant using a strong electric field and accelerated using charged #electrodes https://spacepropulsion.mit.edu/electric-propulsion
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Liquid and solid propellant 🔥 #rocket engines feature low mass efficiency due to the thermodynamic limitations and extremely low efficiency at small thrust. The electric 🔋 thrusters do not pose limits on the propellant exhaust velocity and the propellant mass consumption may be very low https://www.nature.com/articles/s41467-017-02269-7
#ElectricPropulsion #PlasmaThruster #IonThruster #HallThruster
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Liquid and solid propellant 🔥 #rocket engines feature low mass efficiency due to the thermodynamic limitations and extremely low efficiency at small thrust. The electric 🔋 thrusters do not pose limits on the propellant exhaust velocity and the propellant mass consumption may be very low https://www.nature.com/articles/s41467-017-02269-7
#ElectricPropulsion #PlasmaThruster #IonThruster #HallThruster