Publication Date:
2019-07-13
Description:
The discharge chambers of mercury ion thrusters are modelled so the principal effects and processes which govern discharge plasma properties and thruster performance are described. The conservation relations for mass, charge and energy when applied to the Maxwellian electron population in the ion production region yield equations which may be made one-dimensional by the proper choice of coordinates. Solutions to these equations with the appropriate boundary conditions give electron density and temperature profiles which agree reasonably well with measurements. It is then possible to estimate plasma properties from thruster design data and those operating parameters which are directly controllable. By varying the operating parameter inputs to the computer code written to solve these equations, perfromance curves are obtained which agree quite well with measurements.
Keywords:
SPACECRAFT PROPULSION AND POWER
Type:
AIAA PAPER 79-2054
,
International Electric Propulsion Conference; Oct 30, 1979 - Nov 01, 1979; Princeton, NJ
Format:
text
