Study on the Thermal Buffer Mass and Phase Change Material for Thermal Control of the Periodically Working Satellite Component
![]() |
Kim, Taig Young
(Department of Mechanical Engineering, Korea Polytechnic University)
Seo, Jung Gi (Korea Advanced Institute of Science and Technology) Hyun, Bum-Seok (Korea Aerospace Research Institute) Cheon, Hyeong Yul (Korea Aerospace Research Institute) Lee, Jang-Joon (Korea Aerospace Research Institute) |
1 | Mills, A., Farid, M. Selman, J. R., and Al-Hallaj, S., "Thermal conductivity enhancement of phase change materials using a graphite matrix," Applied Thermal Engineering, Vol.26, 2006, pp.1652-1661. DOI |
2 | Gilmore, D. G., Spacecraft Thermal Control Handbook, Volume I: Fundamental Technologies, 2nd Ed., 2002, The Aerospace Press, ElSegundo. |
3 | Kim, T. Y., "Heat capacity estimation of the thermal buffer mass for temperature control of satellite electronic components in periodic operation," Aerospace Science and Technology, Vol.30, 2013, pp.286-292. DOI |
4 | Kim, T. Y., Hyun, B., Lee, J., and Rhee, J., "Numerical study of the spacecraft thermal control hardware combining solid-liquid phase change material and a heat pipe," Aerospace Science and Technology, Vol.27, 2013, pp.10-16. DOI |
5 | Kumar, A., Sekar, A., Siddhartha, D.N., and Govinda, K. V., "Phase change materials (PCM) for thermal control during spacecraft transportation," International Journal of Mechanical and Industrial Engineering, Vol.3, 2013, pp.28-32. |
![]() |