Closed-Loop Thrust and Pressure Profile Throttling of a Nitrous Oxide/Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor
Hybrid motors that employ non-toxic, non-explosive components with a liquid oxidizer and a solid hydrocarbon fuel grain have inherently safe operating characteristics. The inherent safety of hybrid rocket motors offers the potential to greatly reduce overall operating costs. Another key advantage of...
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| Format: | Others |
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DigitalCommons@USU
2012
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| Online Access: | https://digitalcommons.usu.edu/etd/1400 https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=2407&context=etd |