Effects of Aluminum Oxide Particles and Gas Properties on the Thermal Response of Solid Rocket Nozzle Liners
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ; 2008 ; Hartford , CT
01.01.2008
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effects of Propellant Gases on Thermal Response of Solid Rocket Nozzle Liners
Online Contents | 2008
|British Library Conference Proceedings | 1995
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