Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-flourine rocket engine
1959
61 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Methane-fuel corrosion in regeneratively cooled rocket-engine combustors
Tema Archive | 1989
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