Thermal Model of MEMS Thruster. Apurva Varia Propulsion Branch Code 597. Overview. Introduction Statement of Problem Approach Results Conclusion. Introduction. Innovative science missions call for nanosatellites that are smaller, low-cost, and efficient.
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Liquid and Gas exhaust products
Heat through Conduction
Heat through liquid H2O2
Heat through gases
Heat through vaporization of liquid water
Heat from radiation
Chamber Sizing Analysis