Electrothermal Hydrazine Thruster (EHT)
GPTKB entity
Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
spacecraft propulsion system
|
| gptkbp:alsoKnownAs |
gptkb:EHT
|
| gptkbp:application |
spacecraft attitude control
satellite station-keeping |
| gptkbp:developedBy |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:firstFlight |
1970s
|
| https://www.w3.org/2000/01/rdf-schema#label |
Electrothermal Hydrazine Thruster (EHT)
|
| gptkbp:principle |
heating hydrazine electrically to produce thrust
|
| gptkbp:propulsion |
hydrazine
|
| gptkbp:specificImpulseVacuum |
220 to 300 seconds
|
| gptkbp:status |
in use
|
| gptkbp:thrust |
0.1 to 1 Newton
|
| gptkbp:type |
electrothermal thruster
|
| gptkbp:usedOn |
geostationary satellites
|
| gptkbp:bfsParent |
gptkb:Yvonne_Brill
|
| gptkbp:bfsLayer |
6
|