Published July 1, 2018 | Version v1
Journal article

Research And Application Of A Satellite Payload Heat Dissipation System

  • 1. Beijing Institute of Spacecraft Environment Engineering, Beijing 100094 (China)

Description

Due to the installation of high power efficient payload heat dissipation instruments, the traditional fan cannot effectively reduce the working temperature of the instruments. It will cause the failure of the test. Therefore, based on the convection heat control method, the simulation and analysis of the model are carried out, and a payload heat dissipation system is built. The correctness of the model and calculation results is verified by experiments, which can effectively guarantee the smooth operation of instrument testing. This conclusion can provide a theoretical reference for other subsequent high-power payload heat dissipation devices. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1757-899X/392/6/062043

Additional details

Publishing Information

Journal Title
IOP Conference Series. Materials Science and Engineering (Online)
Journal Volume
392
Journal Issue
6
Journal Page Range
[7 p.]
ISSN
1757-899X

Conference

Title
International Conference on Manufacturing Technology, Materials and Chemical Engineering (MTMCE)
Dates
22-24 Jun 2018
Place
Zhuhai (China)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
52094265
Subject category
S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
BLOWERS; COMPUTERIZED SIMULATION; CONVECTION; COOLING; ENERGY LOSSES; EQUIPMENT; HEAT; OPERATION; SATELLITES; TESTING; THERMAL DIFFUSIVITY; THERMAL EFFLUENTS
Descriptors DEC
ENERGY; ENERGY TRANSFER; HEAT TRANSFER; LOSSES; MASS TRANSFER; PHYSICAL PROPERTIES; SIMULATION; THERMODYNAMIC PROPERTIES