Assessing Oxidizer Injector Design via Thermochemical Imaging of PMMA Combustion in a Hybrid Rocket Motor Geometry
AIAA Propulsion and Energy 2020 Forum
01.01.2020
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Variable-flow hybrid rocket oxidizer injector
AIAA | 2001
|The Effects of Oxidizer Injector Design on Hybrid Rockets Combustion Stability
British Library Conference Proceedings | 2006
|