Disclosed is artificial satellite including: a mounting structure supporting equipment-bearing walls; a launcher-adapter rigidly connected to the mounting structure; a first radiator; and at least one first system for transporting heat by a fluid, including at least one duct having a first heat-exchange section and a second heat-exchange section, the second heat-exchange section being capable of being in thermal contact with the first radiator. The first heat-exchange section is in thermal contact with at least one portion of the launcher-adapter. Also disclosed is a method for filling a tank of propellant gas of the artificial satellite.
ARTIFICIAL SATELLITE AND METHOD FOR FILLING A TANK OF PROPELLENT GAS OF SAID ARTIFICIAL SATELLITE
2017-12-21
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Artificial satellite and method for filling a tank of propellent gas of said artificial satellite
Europäisches Patentamt | 2018
|Solid propellent motor for third stage of satellite launcher
Engineering Index Backfile | 1967
|High Temperature Propellent Reactions
Emerald Group Publishing | 1952
|Choice of propellent for cold gas propulsion system for satellite
Engineering Index Backfile | 1965
|Europäisches Patentamt | 2016
|