Arb853
发表于 2025-3-25 03:44:47
Thermal Analysis Technology,ctional and physical characteristics). In the design verification stage, the thermal model is correlated with the results of ground thermal balance test, and the flight performance is further predicted. While being verified by test, the thermal analysis also validates the thermal design.
entice
发表于 2025-3-25 07:38:07
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CON
发表于 2025-3-25 14:33:27
Introduction,y system, the TT&C system, the data management system and the payload system, constitutes the spacecraft. The thermal control technology serves for the whole spacecraft and other systems. Therefore, it is the generic technology of spacecraft engineering.
Meditative
发表于 2025-3-25 17:19:02
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壁画
发表于 2025-3-25 20:43:34
Design of Spacecraft Thermal Control Subsystem,ds to which the spacecraft is exposed in the whole life cycle, to systematically take thermal control measures to organize the heat exchange processes inside and outside the spacecraft so as to keep the temperature of onboard equipments, structures and living environment within the prescribed limits
angina-pectoris
发表于 2025-3-26 03:37:38
Typical Thermal Control Technologies for Spacecraft,hnology, temperature measurement and thermal control technology, etc. Among them, heat transfer technology involves thermal conductive materials, heat pipes, thermal interface materials, thermal control coatings, fluid loops, convection ventilation devices, radiators, consumptive heat dissipating de
音乐等
发表于 2025-3-26 06:04:54
Thermal Analysis Technology,rification and in-orbit technical support. In the design phase, thermal analysis is the most important means to determine the configuration (i.e., functional and physical characteristics). In the design verification stage, the thermal model is correlated with the results of ground thermal balance te
LATER
发表于 2025-3-26 08:30:18
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巡回
发表于 2025-3-26 12:47:06
Typical Thermal Control Design Cases of Spacecraft,The basic thermal control principles, methods and common thermal control technologies of the spacecraft have been thoroughly demonstrated in the aforesaid chapters. This chapter further introduces the applications of these principles, technologies and methods in the thermal control of the spacecraft and parts based on the aforesaid.
先行
发表于 2025-3-26 19:05:58
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