A satellite is disclosed comprising an anti-nadir panel having a first side and a second side. In one or more embodiments, the first side of the anti-nadir panel is mounted to an anti-nadir side of the main body of the satellite. The satellite further comprises at least one battery pack mounted to the second side of the anti-nadir panel, where at least one battery pack comprises at least one battery cell.
Spacecraft with anti nadir battery radiator
2017-07-05
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
Engineering Index Backfile | 1968
|NTRS | 2012
|