Hall effect thruster

GPTKB entity

Statements (56)
Predicate Object
gptkbp:instanceOf gptkb:satellite
electric propulsion device
gptkbp:advantage high efficiency
low thrust
long operational life
erosion of channel walls
gptkbp:alternativeTo Hall-effect thruster
chemical rocket
gptkbp:category gptkb:satellite
electric propulsion
plasma propulsion
gptkbp:component anode
cathode
discharge channel
magnetic coil
power processing unit
gptkbp:developedBy gptkb:NASA
gptkb:Aerojet_Rocketdyne
gptkb:Safran_Aircraft_Engines
gptkb:Busek
gptkb:OKB_Fakel
gptkbp:effect up to 60%
https://www.w3.org/2000/01/rdf-schema#label Hall effect thruster
gptkbp:introducedIn gptkb:Soviet_Union
gptkbp:inventedBy gptkb:Yevgeny_Morozov
1960s
gptkbp:operates accelerating ions
using Lorentz force
gptkbp:operatingPower hundreds of watts to tens of kilowatts
gptkbp:operatingSystem 200–2000 V
gptkbp:propulsion gptkb:krypton
gptkb:xenon
gptkbp:relatedTo gptkb:gridded_ion_thruster
gptkb:VASIMR
gptkb:magnetoplasmadynamic_thruster
Hall-effect thruster
arcjet
electrospray thruster
pulsed plasma thruster
gptkbp:specificImpulseVacuum 1500–2500 s
gptkbp:thrust tens to hundreds of millinewtons
gptkbp:usedIn satellites
interplanetary missions
space probes
orbit raising
spacecraft station-keeping
gptkbp:usedOn gptkb:BepiColombo
gptkb:Dawn_spacecraft
gptkb:SMART-1
gptkb:SES-17
gptkb:AEHF_satellites
gptkbp:uses magnetometer
electric field
ionized propellant
gptkbp:bfsParent gptkb:Robert_N._Hall
gptkbp:bfsLayer 6