Ceramic Matrix Composite as Liners for Improved Ablative Chambers
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ; 2009 ; Denver , Colorado
01.01.2009
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Development of Composite Ablative Liners for Solid Rocket Motor Flex Nozzles
Online Contents | 2013
|Ribbed Coolant Liners for Combustion Chambers
NTRS | 1984
|Design of ablative thrust chambers and their materials
AIAA | 1964
|