The invention relates to a spacecraft comprising: a frame (4), an electrical device (1) supplied and/or controlled by electric cables, and an orientation system for orienting the electrical device (1), the orientation system comprising: - at least two rotary actuators (2a, 2b) with non-parallel axes (Δa, Δb), - a joining piece (5) between the two rotary actuators, one of the actuators (2a) being connected to the electrical device (1) and to the joining piece (5), the other actuator (2b) being connected to the joining piece (5) and to the frame (4) of the spacecraft, - one or more guide forks (6) that are arranged on the outside of the joining piece (5) and fastened to the latter, each guide fork comprising fingers (9a, 9b, 9c) configured to support the electric cables and to form a guide path for the cables such that the electric cables never exert, on the rotary actuators (2a, 2b), a torque greater than the torque capacity of the actuators.
ENGIN SPATIAL COMPRENANT UN DISPOSITIF ÉLECTRIQUE ET UN SYSTÈME D'ORIENTATION DUDIT DISPOSITIF ÉLECTRIQUE
SPACECRAFT COMPRISING AN ELECTRICAL DEVICE AND AN ORIENTATION SYSTEM FOR SAID ELECTRICAL DEVICE
RAUMFAHRZEUG MIT EINER ELEKTRISCHEN VORRICHTUNG UND AUSRICHTUNGSSYSTEM FÜR DIE ELEKTRISCHE VORRICHTUNG
2024-03-13
Patent
Elektronische Ressource
Französisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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