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 D1 in a +Y direction from a satellite gravity center (101) to the first thruster group and a second distance D2 in a −Y direction from the satellite gravity center to the second thruster group becomes inverse to a ratio between the first operating number and the second operating number.
ARTIFICIAL SATELLITE AND SATELLITE PROPULSION METHOD
2019-10-03
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Satellite/spacecraft propulsion
NTRS | 1991
|Small Satellite Propulsion Options
NTIS | 1994
|