Identification of radiative heat transfer parameters in multilayer thermal insulation of spacecraft

Autor: Aleksey V. Nenarokomov, S. A. Budnik, Oleg M. Alifanov, Irina V. Krainova, Leonid A. Dombrovsky
Rok vydání: 2017
Předmět:
Zdroj: International Journal of Numerical Methods for Heat & Fluid Flow. 27:598-614
ISSN: 0961-5539
DOI: 10.1108/hff-03-2016-0136
Popis: Purpose The purpose of this study is to optimize multilayer vacuum thermal insulation (MLI) of modern high-weight spacecrafts. An adequate mathematical simulation of heat transfer in the MLI is impossible if there is no available information on the main insulation properties. Design/methodology/approach The results of experiments in thermo-vacuum facilities are used to re-estimate some radiative properties of metallic foil/metalized polymer foil and spacer on the basis of the inverse problem solution. The experiments were carried out for the sample of real MLI used for the BP-Colombo satellite (ESA). The recently developed theoretical model based on neglecting possible near-field effects in radiative heat transfer between closely spaced aluminum foils was used in theoretical predictions of heat transfer through the MLI. Findings A comparison of the computational results and the experimental data confirms that there are no significant near-field effects between the neighboring MLI layers. It means that there is no considerable contradiction between the far-field model of radiative transfer in MLI and the experimental estimates. Originality/value An identification procedure for mathematical model of the multilayer thermal insulation showed that a modified theoretical model developed recently can be used to estimate thermal properties of the insulation at conditions of space vacuum.
Databáze: OpenAIRE