Development of a Cold Gas Propulsion System for the ... - SSL - MIT
Development of a Cold Gas Propulsion System for the ... - SSL - MIT
Development of a Cold Gas Propulsion System for the ... - SSL - MIT
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If 1D isentropic flow is assumed, <strong>the</strong> pressure and Mach number <strong>of</strong> <strong>the</strong> gas at any point in a nozzle can<br />
be related to <strong>the</strong> stagnation or chamber pressure. There<strong>for</strong>e: