A spacecraft chassis includes a chassis body defined by first and second opposing sides bound by a perimeter, wherein at least one heat-generating component is configured to be secured directly to the chassis body, and at least one heat dissipating feature configured to radiate heat generated from the at least one heat-generating component into outer space.
Spacecraft chassis and component configuration
2023-12-05
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |