Application of combined heat transfer models for designing thermal protection systems of reusable launch vehicles
Published: 18.12.2012
Authors: Dylko YU.B., Prosuntsov P.V.
Published in issue: #9(9)/2012
DOI: 10.18698/2308-6033-2012-9-370
Category: Engineering | Chapter: Rocket and space technology
Sorry, this page is not available in English