The invention discloses a
radiant cooling plate
assembly applied to a space pump drive fluid loop
system. The
assembly comprises three or more odd number of
radiant cooling plate single plates, and the central
radiant cooling plate
single plate is fixedly connected with a
spacecraft body; each
single plate comprises a frame, a rigid fluid pipeline and a flexible
radiation film, the rigid fluid pipeline is composed of a liquid inlet main pipeline, a liquid return main pipeline and a plurality of parallel
branch pipelines and cooperates with the frame to form a supporting structure, and the flexible
radiation film covers the pipelines and is used for
radiation heat dissipation. In the launching stage, all the single plates are stacked and folded and locked to a
spacecraft body through a pressing and releasing mechanism. In the on-
orbit stage, after the pressing and releasing mechanism is unlocked, the single plates are unfolded in different time sequences through the on-
orbit unfolding mechanism, and finally the single plates are symmetrically distributed with the center line of the central
single plate as the symmetry axis and are kept coplanar. Through the design of the symmetrical configuration, the rigid-flexible
composite structure and the parallel flow channels, the envelope adaptability of the launching stage and the heat dissipation efficiency and the
structural stability of the on-
orbit stage are considered, and the
heat management requirement of the high-power
spacecraft is met.