MORPHOLOGY AND ANTI-ABLATION PROPERTIES OF COMPOSITES NOZZLES UNDER THE 100MM H202- PE HYBRID ROCKET MOTOR TEST
IAF Materials and Structures Symposium ; 2020 ; Online
2021
Aufsatz (Konferenz)
Englisch
Performance of Dicyclopentadiene/H202-Based Hybrid Rocket Motors with Metal Hydride Additives
Online Contents | 2013
|Erosion in rocket motor nozzles
Tema Archiv | 1977
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AIAA | 2019
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