Thrust Augmented Nozzle for a Hybrid Rocket with a Helical Fuel Port
A thrust augmented nozzle for hybrid rocket systems is investigated. The design lever-ages 3-D additive manufacturing to embed a helical fuel port into the thrust chamber of a hybrid rocket burning gaseous oxygen and ABS plastic as propellants. The helical port significantly increases how quickly th...
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| Format: | Others |
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DigitalCommons@USU
2018
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| Online Access: | https://digitalcommons.usu.edu/etd/6915 https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=8018&context=etd |