Catalytic and radiative properties in the thermal protection of spacecraft.

Аuthors

Kuprukhin A. A.^*, Nikitin P. V.^**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: kupryukhin@mail.ru
**e-mail: petrunecha@gmail.com

Abstract

The paper presents a method of experimental determination of catalytic and radia-tive properties of advanced materials for thermal protection of spacecraft gliding class. The method was developed for use in the high-gas-dynamic stands reproducing full-scale thermal parameters during the flight of the spacecraft (spacecraft) in the atmosphere of the Earth and other planets. The influence of catalytic and radiative properties on heat transfer on the surface of spacecraft.

Keywords:

thermodynamics, heat and mass transfer, thermal protection, heterogeneous flow, zone of mixed uses coatings, thermal protection materials

Download