magnetoplasmadynamic thruster
GPTKB entity
Statements (41)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
electric propulsion device
|
| gptkbp:advantage |
high thrust-to-weight ratio
electrode erosion high exhaust velocity requires high power |
| gptkbp:alsoKnownAs |
MPD thruster
|
| gptkbp:application |
deep space missions
satellite station-keeping interplanetary propulsion |
| gptkbp:canUsePropellant |
gptkb:argon
gptkb:xenon hydrogen lithium |
| gptkbp:category |
gptkb:satellite
electric propulsion plasma propulsion |
| gptkbp:developedBy |
1960s
researchers in the United States researchers in the Soviet Union |
| gptkbp:firstTestMatch |
1960s
|
| gptkbp:hasComponent |
gptkb:battery
anode cathode magnetic field generator |
| https://www.w3.org/2000/01/rdf-schema#label |
magnetoplasmadynamic thruster
|
| gptkbp:notableMission |
Japanese Space Flyer Unit
NASA 2001 Deep Space Test |
| gptkbp:operates |
gptkb:Lorentz_force
|
| gptkbp:produces |
ionized plasma jet
|
| gptkbp:relatedTo |
Hall-effect thruster
|
| gptkbp:requires |
vacuum environment
|
| gptkbp:testedBy |
gptkb:NASA
gptkb:Space_Shuttle gptkb:JAXA Japanese satellites |
| gptkbp:usedIn |
gptkb:satellite
|
| gptkbp:uses |
gptkb:plasma
magnetic fields electric currents |
| gptkbp:bfsParent |
gptkb:Hall-effect_thruster
|
| gptkbp:bfsLayer |
5
|