Hybrid rockets with mixed N2O/CO2 oxidizers for Mars Ascent Vehicles
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DOI: 10.1016/j.actaastro.2020.05.060
Abstract: Abstract The objective of this research is to demonstrate the feasibility of sustained combustion in hybrid rocket motor configuration with oxidizers containing high concentrations of C O 2 , an in situ propellant suitable for… read more here.
Keywords: co2 oxidizers; mixed n2o; rockets mixed; oxidizers mars ... See more keywords