Abstract
A numerical study of three-dimensional effects on the performance of a micronozzle fabricated from e at silicon wafers is performed by use of both continuum and kinetic approaches. The nozzle operates in a low-Reynoldsnumber regime, and viscous effects dominate the gas expansion. Thrust losses occur because the shear on the wall is greater in a e at nozzle cone guration than in an axisymmetric conical nozzle. Therefore, the prediction of the micronozzle performance based on axisymmetric or two-dimensional modeling can lead to signie cant design errors.Comparisonofsimulationwithrecentdatashowsgood agreementintermsofthrustpredictionsforcold-gas thrusters at Reynolds numbers of approximately 2 ££ 102.
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