Ion Propulsion for Space Flight
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:space_propulsion_technology
|
| gptkbp:advantage |
efficient fuel usage
low acceleration |
| gptkbp:appliesTo |
gptkb:satellite
|
| gptkbp:contrastsWith |
chemical propulsion
|
| gptkbp:developedBy |
gptkb:NASA
|
| gptkbp:enables |
long-duration space missions
|
| gptkbp:firstTestMatch |
1960s
|
| gptkbp:operatesIn |
vacuum of space
|
| gptkbp:produces |
low thrust
|
| gptkbp:provides |
high specific impulse
|
| gptkbp:relatedTo |
gptkb:gridded_ion_thruster
gptkb:Hall-effect_thruster |
| gptkbp:requires |
electrical power
|
| gptkbp:usedFor |
interplanetary missions
|
| gptkbp:usedIn |
gptkb:Deep_Space_1
gptkb:Dawn_spacecraft |
| gptkbp:uses |
gptkb:Hall-effect_thruster
electric propulsion xenon propellant |
| gptkbp:bfsParent |
gptkb:Ernst_Stuhlinger
|
| gptkbp:bfsLayer |
5
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ion Propulsion for Space Flight
|