Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:plasma_rocket_engine
|
| gptkbp:application |
space propulsion
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:demonstratedContinuousOperation |
2010
|
| gptkbp:designedBy |
gptkb:Franklin_Chang_Díaz
|
| gptkbp:firstTestMatch |
2009
|
| gptkbp:hasFacility |
Ad Astra Rocket Company laboratory, Houston, Texas
|
| gptkbp:manufacturer |
gptkb:Ad_Astra_Rocket_Company
|
| gptkbp:maximumSpeed |
200 kW
|
| gptkbp:propulsion |
gptkb:argon
gptkb:xenon |
| gptkbp:relatedTo |
VASIMR engine family
|
| gptkbp:specificImpulseVacuum |
5000 s
|
| gptkbp:status |
experimental
|
| gptkbp:technology |
VASIMR (Variable Specific Impulse Magnetoplasma Rocket)
|
| gptkbp:thrust |
5.4 N
|
| gptkbp:website |
https://www.adastrarocket.com/vx-200/
|
| gptkbp:bfsParent |
gptkb:Ad_Astra_Rocket_Company_Costa_Rica
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
VASIMR VX-200 engine
|