Analysis of the features of the implementation of the launch unit flight scheme for micro spacecraft injections in an intermediate orbit with synchronous precession
Published: 26.09.2019
Authors: Zelvin D.A., Toporkov A.G.
Published in issue: #9(93)/2019
DOI: 10.18698/2308-6033-2019-9-1918
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control