Method of computing manoeuvres parameters during the space flight into the libration point L2 of the Sun - Earth system
Published: 19.05.2017
Authors: Ponomareva I.A.
Published in issue: #7(67)/2017
DOI: 10.18698/2308-6033-2017-7-1641
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control