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We establish the original cold-flow approach to predict characteristic velocity and specific impulse of bipropellant thrusters. The accuracy is quantitatively evidenced by comparing with corresponding combustion tests.
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This page is a summary of: Direct Formulation of Bipropellant Thruster Performance for Quantitative Cold-Flow Diagnostic, Journal of Propulsion and Power, July 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b38310.
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