Disclosed is a spacecraft including: a housing defining an exterior space, the housing having a first face and a second face; and first and second radiators carried by the first and second faces, the first and second radiators each having an inner main face, an outer main face, and side faces. The spacecraft includes a first auxiliary radiator and a first auxiliary heat transfer device thermally connecting the first auxiliary radiator to the inner main face of the second radiator, the first auxiliary radiator being arranged in a first portion of the exterior space defined by the outer main face of the first radiator and by first planes containing the side faces of the first radiator. The first auxiliary heat transfer device includes a heat conducting device. The first auxiliary radiator is composed solely of one or two radiating panels supporting the heat conducting device.
ENGIN SPATIAL
SPACE VEHICLE
RAUMFAHRZEUG
2019-09-04
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS |