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Some Peculiarities in the Use of a Single Vector Algorithm for Determination of Artificial | 39 |
Determination of the Aerodynamic Characteristics of a Satellite with Consideration | 48 |
Possible Effects of Plasma Turbulence in the Vicinity of Diurnal Polar CuspsV A Gudkova | 54 |
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according altitude analysis angle angular approximation assumed atmosphere axis boundary calculated characteristics coefficient component computed conducted considered constant coordinate corresponding cosmic rays curve density dependence detector determined direction distance distribution earth effect electron energy engine equal equations errors estimate experiment experimental factor field Figure flight flux frequency function given height increase indicated initial integral intensity interval layer limits lunar magnetic Mars matrix maximum means measurements method motion noted observed obtained operation orbit orientation Original parameters particles period phase plane plasma position possible presented problem protons publisher radiation range recording region relative respect Russian satellite shown shows solar solution space spectrum surface Table temperature tion trajectory transmitted units values variation vector vehicle velocity wave wind