DETERMINATION OF THE STRESS-STRAIN STATE OF THE PROTECTION OF LAUNCHER ELEMENTS FROM GAS-DYNAMIC IMPACT DURING ROCKET LAUNCH
Author: Akimov D., «Yuzhnoye» State Design Office
Section: Strength of rocket structures, vibrations, acoustic waves and noise effects
Publication date: 24 April, 2026
DOI: HTTP://DOI.ORG/10.62717/3083-7057-2026-1-001
ORCID: https://orcid.org/0000-0002-5881-589X