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Assessment was made by calculations for the possible consequences of the effect of plasma plume injected by the solar electric propulsion system (SEPS) on the structural components of “Phobos-Soil” spacecraft (SC). Propulsion system comprises three SPT-140 thrusters, two of which should secure the required total thrust impulse during 8000hours of operation approximately. Variation of the solar panel...
An adequate physical model for the ablative pulsed plasma thrusters (APPT) processes was developed as a result of complex theoretical and experimental studies conducted by RIAME for the processes of plasma acceleration in the APPT and determination of plasma parameters, electric currents, magnetic fields, volumetric electromagnetic forces inside and outside the discharge channel. Possibility for reaching...
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