Abstract:The new generation of intelligent satellites is now in urgent demand for bipropellant thrusters in minimum impulse mode without limitation. Thruster's impulse performance involving combustion efficiency and impulse repeatability strongly correlates to transient spray atomization. Accordingly, the transient spray atomization under impulse working condition is investigated to optimize thruster dynamic response. In order for thrusters to work reliably in short-impulse mode and to further improve its impulse repea… Show more
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