Thermal control louvers for CubeSats or small spacecraft may include a plurality of springs attached to a back panel of the thermal control louvers. The thermal control louvers may also include a front panel, which includes at least two end panels interlocked with one or more middle panels. The front panel may secure the springs, shafts, and flaps to the back panel.
CubeSat form factor thermal control louvers
2018-01-09
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
CubeSat Form Factor Thermal Control Louvers
NTRS | 2018
|MEMS Louvers for Thermal Control
British Library Conference Proceedings | 1999
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