When a first operating number being the number of thrusters in a first thruster group (115) that are operated and a second operating number being the number of thrusters in a second thruster group (125) that are operated are different, a ratio between a first distance Din a +Y direction from a satellite gravity center (101) to the first thruster group (115) and a second distance Din a -Y direction from the satellite gravity center (101) to the second thruster group (125) becomes inverse to a ratio between the first operating number and the second operating number.
SATELLITE, AND SATELLITE PROPULSION METHOD
SATELLIT UND SATELLITENANTRIEBSVERFAHREN
SATELLITE ET PROCÉDÉ DE PROPULSION DE SATELLITE
07.04.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Satellite/spacecraft propulsion
NTRS | 1991
|NTRS | 2015
|Satellite/Spacecraft Propulsion
NTIS | 1991
|