Optimization of the spacecraft final orbit and the trajectory of the apsidal impulse launch, with due regard to spent stage jettisons into the atmosphere
Published: 26.04.2019
Authors: Grigoriev I.S., Proskuryakov A.I
Published in issue: #4(88)/2019
DOI: 10.18698/2308-6033-2019-4-1869
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control