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/392/6/062043Additional details
Identifiers
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