Hydrogen film cooling of a small hydrogen-oxygen thrust chamber and its effect on erosion rates of various ablative materials
NASA technical paper ; 1098
NASA Lewis Research Center report ; E-8909
Report / E ; 8909
1977
25 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Ablative Thrust Chamber Feasibility
NTIS | 1963
Experimental and simulation study of a Gaseous oxygen/Gaseous hydrogen vortex cooling thrust chamber
Online Contents | 2016
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