Results 101 to 110 of about 9,251 (208)

13kW Advanced Electric Propulsion Flight System Development and Qualification [PDF]

open access: yes
The next phase of robotic and human deep space exploration missions requires high performance, high power solar electric propulsion systems for large-scale science missions and cargo transportation.
Barber, Matthew   +6 more
core   +1 more source

In-orbit demonstration of an iodine electric propulsion system. [PDF]

open access: yesNature, 2021
Rafalskyi D   +10 more
europepmc   +1 more source

Recent advances in MPD thruster research at Princeton [PDF]

open access: yes
A summary of last years anode, plasma, and cathode findings is presented. A summary of this years activities and findings is also presented. A brief discussion of previous and current understanding is given and covers the following topics: existence of ...
Choueiri, Edgar Y., Jahn, Robert G.
core   +1 more source

High power Hall thrusters [PDF]

open access: yes35th Joint Propulsion Conference and Exhibit, 1999
Robert Jankovsky   +2 more
openaire   +1 more source

MPD thruster technology [PDF]

open access: yes
MPD (MagnetoPlasmaDynamic) thrusters demonstrated between 2000 and 7000 seconds specific impulse at efficiencies approaching 40 percent, and were operated continuously at power levels over 500 kW.
Lapointe, Michael R.   +2 more
core   +1 more source

Mission to Psyche: Including Undergraduates and the Public on the Journey to a Metal World. [PDF]

open access: yesSpace Sci Rev, 2023
Bowman CDD   +22 more
europepmc   +1 more source

Completion of the Long Duration Wear Test of the NASA HERMeS Hall Thruster [PDF]

open access: yes
The NASA Hall Effect Rocket with Magnetic Shielding (HERMeS) 12.5-kW Hall thruster has been the subject of extensive technology maturation by NASA GRC and JPL in preparation for development into a flight propulsion system.
Frieman, Jason D.   +7 more
core   +1 more source

Electric thruster research [PDF]

open access: yes
It has been customary to assume that ions flow nearly equally in all directions from the ion production region within an electron-bombardment discharge chamber. In general, the electron current through a magnetic field can alter the electron density, and
Kaufman, H. R., Robinson, R. S.
core   +2 more sources

High Voltage Hall Accelerator Propulsion System Development for NASA Science Missions [PDF]

open access: yes
NASA Science Mission Directorates In-Space Propulsion Technology Program is sponsoring the development of a 3.8 kW-class engineering development unit Hall thruster for implementation in NASA science and exploration missions.
Dankanich, John   +7 more
core   +1 more source

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