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2: Ideal mixture ratio & specific impulse values and compounds'densities[7]

2: Ideal mixture ratio & specific impulse values and compounds'densities[7]

Source publication
Technical Report
Full-text available
The aim of the following report is to present a different set of solutions for a bi-propellant propulsion system of a 250 kg dry mass spacecraft’s kick-stage engine capable of performing a velocity variation of 2500 m/s. This analysis has been carried out considering two different propulsion couples. The first propulsion couple taken into account h...