Research and development of heat flux sensor for ablative thermal protection of spacecrafts

•An approach to solve boundary inverse heat transfer problem for combined conductive-thermokinetic process is suggested.•A new technology for heat flux sensors is proposed.•Sensors can be installed in flexible thermal protection of re-entry vehicles. The objective of this paper is to estimate heat f...

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Veröffentlicht in:	International journal of heat and mass transfer 2016-06, Vol.97, p.990-1000
Hauptverfasser:	Nenarokomov, A.V., Alifanov, O.M., Budnik, S.A., Netelev, A.V.
Format:	Artikel
Sprache:	eng
Schlagworte:	Ablation Ablative thermal protection Fluxes Heat flux Heat flux sensors Heat transfer Inverse problems Mathematical analysis Re-entry spacecraft Research and development Spacecraft Thermal protection
Online-Zugang:	Volltext
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