Statements (53)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
Electric propulsion device
|
| gptkbp:advantage |
High efficiency
Complex power electronics Long operational life Low propellant consumption Low thrust Magnetic field erosion |
| gptkbp:alternativeTo |
Chemical rockets
Ion thrusters |
| gptkbp:category |
Electric propulsion
Plasma propulsion Spacecraft propulsion |
| gptkbp:component |
Magnetic field
Plasma Anode Cathode Discharge channel |
| gptkbp:firstFlight |
1971
|
| https://www.w3.org/2000/01/rdf-schema#label |
Hall effect thrusters
|
| gptkbp:introducedIn |
gptkb:Meteor_satellite
|
| gptkbp:inventedBy |
gptkb:Soviet_Union
1960s |
| gptkbp:notableModel |
BPT-4000
HET-300 SPT-100 TAL (Thruster with Anode Layer) Xenon Hall Thruster |
| gptkbp:principle |
gptkb:Hall_effect
Electromagnetic acceleration |
| gptkbp:propulsion |
gptkb:Krypton
gptkb:Xenon |
| gptkbp:relatedTo |
Electromagnetic thrusters
Electrostatic thrusters Ion thrusters Magnetoplasmadynamic thrusters Plasma engines |
| gptkbp:specificImpulseVacuum |
1000–3000 seconds
|
| gptkbp:thrust |
millinewtons to newtons
|
| gptkbp:usedBy |
gptkb:NASA
gptkb:SpaceX gptkb:Boeing gptkb:Roscosmos gptkb:ESA gptkb:ISRO |
| gptkbp:usedIn |
Spacecraft propulsion
|
| gptkbp:usedOn |
communications satellites
Earth observation satellites deep space missions interplanetary probes station-keeping orbit raising |
| gptkbp:bfsParent |
gptkb:PEPL_(Plasmadynamics_and_Electric_Propulsion_Laboratory)
|
| gptkbp:bfsLayer |
7
|