Experimental Investigation of N2O/O2 Mixtures as Volumetrically Efficient Oxidizers for Small Spacecraft Hybrid Propulsion Systems
A hybrid thruster system utilizes propellants in two different stages, traditionally a solid fuel and a gaseous or liquid oxidizer. Recently hybrid thrusters have become a popular topic of research due to the high demand of a ”green” replacement for hydrazine. Not only are hybrid thruster systems ty...
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| Format: | Others |
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DigitalCommons@USU
2019
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| Online Access: | https://digitalcommons.usu.edu/etd/7690 https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=8826&context=etd |