Cosmic Research, Том 18

a₁ accuracy algorithm altitude angle angular angular velocity approximation assume atmosphere axis boundary bursts calculated carrier rockets center of mass characteristics coefficient component concentration coordinate corresponding curve decrease density dependence determined earth electrons energy equations errors estimate experimental flight flux function geomagnetic Geophys gyroscopes height heterosphere increase initial ionosphere ions Issled km/sec Kosm Kosmicheskie Issledovaniya latitude launch layer Luna 24 magnetic field magnetopause magnetosphere Mars Martian mass maximum measurements method minimum Moscow motion observed obtained optimal optimal control optimum orbit Original article submitted Oxyz ozone parameters particles perturbations photolysis plane planetokhod plasma plasmasphere problem proton r₁ radiation radius region relative rocket rotation Russian satellite solar wind solution spacecraft spectra spectrum surface temperature Tiksi tion trajectory transfer Translated from Kosmicheskie values variations vector velocity Venus