Patent application number | Description | Published |
20080217483 | THERMAL CONTROL DEVICE ON BOARD A SPACECRAFT - The invention relates to a thermal control device intended to dissipate the heat generated by a payload on a spacecraft, comprising a number of surfaces and including means for circulating a refrigerant. An evaporation zone (Z | 09-11-2008 |
20100213319 | Craft and Method of Coupling a Propulsion System to a Regenerative Fuel Cell System - The invention relates to a craft comprising an energy storage system of the RFCS (regenerative fuel cell system) type and a system for pressurizing the propellants used for propulsion. The craft also comprises a plurality of means ( | 08-26-2010 |
20100223942 | Thermal Management Device for a Spacecraft - The invention relates to a thermal management device intended to collect the heat dissipated by a group of dissipative equipment of a spacecraft in an evaporation zone before discharging this heat to cold space via a condensation zone, situated in the region of the radiators. The evaporation zone and the condensation zone each consist of at least one heat-exchange part comprising a network of a plurality of compact heat-exchange elements distributed over their respective heat-exchange surface and connected in series and/or in parallel by the tubes of the thermal fluid circulation means. | 09-09-2010 |
20160001896 | SATELLITE WITH VARIABLE MASTER CROSS SECTION - A satellite comprises at least one first communication module, a repeater module, one or more antennas, at least one propulsion module and an avionics module, the repeater module comprising: a north first panel when the satellite is in an orbital position, an east second panel, a south third panel and a west fourth panel arranged respectively opposite the north first panel and the east second panel, the north panel and the south panel having widths Xmc | 01-07-2016 |