Optimization of the trajectory of the spacecraft insertion into the system of heliocentric orbits
Crossref DOI link: https://doi.org/10.1134/S0010952517020034
Published Online: 2017-06-01
Published Print: 2017-05
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Konstantinov, M. S.
Thein, Min
License valid from 2017-05-01