Combustion possibility assessment for separating launch-vehicle components during atmospheric phase of descent trajectory-Reference-Cited by-同舟云学术

Combustion possibility assessment for separating launch-vehicle components during atmospheric phase of descent trajectory

Published:2019-06 Issue: Volume:159 Page:540-546
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Trushlyakov V.,Zharikov K.^ORCID,Davydovich D.^ORCID

Funder

Development of scientific-technical fundamentals of the combustion of the separated elements of space rockets with the goal of reducing the impact areas

Publisher

Elsevier BV

Subject

Aerospace Engineering

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