A method of forming a spacecraft adapter layout to meet the requirements of dynamic compatibility by topological and parametric optimization methods
Published: 10.12.2021
Authors: Borovikov A.A., Tushev O.N.
Published in issue: #12(120)/2021
DOI: 10.18698/2308-6033-2021-12-2134
Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft