AXISYMMETRIC AIR AUGMENTED METHANOL/GOX ROCKET MIXING DUCT EXPERIMENTAL THRUST STUDY
A hot-flow axisymmetric Air Augmented Rocket (AAR) test apparatus was constructed to test various mixing duct configurations at static conditions. Primary flow for the AAR was provided through a liquid methanol-gaseous oxygen bipropellant rocket. Experimental thrust measurements were recorded and pr...
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| Format: | Others |
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DigitalCommons@CalPoly
2013
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| Online Access: | https://digitalcommons.calpoly.edu/theses/930 https://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=1984&context=theses |