Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
plasma rocket engine
|
| gptkbp:application |
space propulsion
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:firstTestMatch |
2009
|
| gptkbp:fullName |
gptkb:Variable_Specific_Impulse_Magnetoplasma_Rocket
|
| https://www.w3.org/2000/01/rdf-schema#label |
VASIMR
|
| gptkbp:inventedBy |
gptkb:Franklin_Chang_Díaz
|
| gptkbp:manufacturer |
gptkb:Ad_Astra_Rocket_Company
|
| gptkbp:potentialMission |
Mars missions
lunar cargo transport |
| gptkbp:powerSource |
200 kW (VX-200 prototype)
|
| gptkbp:propulsion |
gptkb:argon
gptkb:xenon hydrogen |
| gptkbp:specificImpulseVacuum |
3000–5000 s (variable)
|
| gptkbp:status |
in development
|
| gptkbp:technology |
magnetic nozzle
radio frequency (RF) plasma heating |
| gptkbp:thrust |
5 N (VX-200 prototype)
|
| gptkbp:website |
https://www.adastrarocket.com/vasimr/
|
| gptkbp:bfsParent |
gptkb:Hall_effect_thruster
|
| gptkbp:bfsLayer |
7
|