Cosmic Research, Том 28

according allowance altitude analysis angle angular approximation assume atmosphere average axis body boundary calculated characteristic coefficient components consider coordinate system corresponding cosmic ray curve decrease density dependence described determined direction distance distribution dynamics Earth effect electron elements energy equal equations error estimate experimental experiments expression field flux force frequency function given increase initial integral interval ionosphere ions issues linear magnetic field mass maximum measurements method Moscow motion observed obtained orbit oscillations parameters particles performed period plane plasma position possible presented probe problem radiation radio range region relations relative respect rotation Russian satellite satisfied shown shows solar wind solution space spacecraft stability structure surface Table temperature tion Translated values variables variations vector velocity waves