A Model has been developed capable of calculating the electrostatic return of spacecraft-emitted molecules that are ionized and attracted back to the spacecraft by the spacecraft electric potential on its surfaces. The return of ionized contaminant molecules to charged spacecraft surfaces is very important to all altitudes. It is especially important at geosynchronous and interplanetary environments, since it may be the only mechanism by which contaminants can degrade a surface. This model is applicable to all altitudes and spacecraft geometries. In addition to results of the model will be completed to cover a wide range of potential space systems.Rantanen, R. and Gordon, T.Marshall Space Flight CenterMATHEMATICAL MODELS; ELECTROSTATICS; ELECTRIC POTENTIAL; CONTAMINANTS; AEROSPACE SYSTEMS; SPUTTERING; CROSS SECTIONS; ELECTRONS; EMITTANCE; SURFACE TEMPERATURE; DEBYE LENGTH
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