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
2021-04-07
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
Satellite/spacecraft propulsion
NTRS | 1991
|NTRS | 2015
|Satellite/Spacecraft Propulsion
NTIS | 1991
|