Analysis of the design of the drag braking device for CubeSat satellites for withdrawal from low near-Earth orbits
Published: 11.05.2020
Authors: Pichkhadze K.M., Sysoev V.K., Firsyuk S.O., Yudin A.D.
Published in issue: #5(101)/2020
DOI: 10.18698/2308-6033-2020-5-1982
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control