Modularized satellite thermal control system capable of realizing high agility maneuvering capability

The invention relates to the technical field of spacecraft thermal control, and discloses a modular satellite thermal control system capable of realizing high agility maneuverability, which comprises heat dissipation modules and connecting modules, and is characterized in that a plurality of heat di...

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Hauptverfasser: WANG TENG, ZHANG GUOBIN, MU YUANDONG, GAO XINGSU, FAN LIJIA, WANG YUE, ZHANG KAN, HE ZHI, LIU YALI, ZU JIAGUO, YANG WENTAO
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creator WANG TENG
ZHANG GUOBIN
MU YUANDONG
GAO XINGSU
FAN LIJIA
WANG YUE
ZHANG KAN
HE ZHI
LIU YALI
ZU JIAGUO
YANG WENTAO
description The invention relates to the technical field of spacecraft thermal control, and discloses a modular satellite thermal control system capable of realizing high agility maneuverability, which comprises heat dissipation modules and connecting modules, and is characterized in that a plurality of heat dissipation modules are connected through the connecting modules to form a polygonal cabin section; the heat dissipation module comprises a main heat dissipation plate, an auxiliary heat dissipation plate and a structural substrate, and the main heat dissipation plate and the structural substrate are oppositely arranged and connected through the auxiliary heat dissipation plate; the structural substrates of the adjacent heat dissipation modules are connected with the connecting modules; the structural substrate is a honeycomb-shaped plate, the embedded heat pipes are arranged in the structural substrate in an orthogonal mode, and the space where the embedded heat pipes are not arranged is filled with a honeycomb stru
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subjects AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
title Modularized satellite thermal control system capable of realizing high agility maneuvering capability
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