Chugging Instability of H2O2 Monopropellant Thrusters with Catalyst Reactivity and Support Sizes

摘要

HIGH-PERFORMING storable propellants such as hydrazinen( ) (amonopropellant) and nitrogen tetroxide (an oxidizer)nin bipropellant systems are currently used despite their toxicity. As anresult of the growing concerns and regulations related to the environ-nment, interest in rocket-grade hydrogen peroxide (one of the oldestnpropellants) as an alternative propellant has grown since the mid-n1990s because of its nontoxic, storable characteristics