Combustion Characteristics of Gas Hybrid Rocket using H2O/HNO3 as Oxidizer
51st AIAA/SAE/ASEE Joint Propulsion Conference
2015-01-01
Conference paper
Electronic Resource
English
Variable-flow hybrid rocket oxidizer injector
AIAA | 2001
|Combustion Characteristics of Gas Hybrid Rocket using H~2O/HNO~3 as Oxidizer (AIAA 2015-4136)
British Library Conference Proceedings | 2015
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