Physical and Mathematical Simulation of Electric Polarization of Low-Orbit Spacecraft under the Conditions of Hypersonic Flow by a Stream of Plasma of the Earth's Upper Ionosphere

Details Physical and Mathematical Simulation of Electric Polarization of Low-Orbit Spacecraft under the Conditions of Hypersonic Flow by a Stream of Plasma of the Earth's Upper Ionosphere Physical and Mathematical Simulation of Electric Polarization of Low-Orbit Spacecraft under the Conditions of Hypersonic Flow by a Stream of Plasma of the Earth's Upper Ionosphere

Jan 2004

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004cosre..42...39s&link_type=abstract

Cosmic Research, v. 42, Issue 1, p. 39-47 (2004).

Physics

Scientific paper

The charging processes in the vicinity of a low-orbital spacecraft
moving in the midlatitude ionosphere are considered. It is shown that
the main feature of charging of such an object is its polarization. The
calculation results are analyzed in the context of general theoretical
concepts.

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