A method for selecting design parameters of a small spacecraft de-orbiting system
Published: 09.08.2020
Authors: Krestina A.V., Tkachenko I.S.
Published in issue: #8(104)/2020
DOI: 10.18698/2308-6033-2020-8-2002
Category: Aviation and Rocket-Space Engineering | Chapter: Design, Construction, Production, Testing, and Operation of Aircraft