Performance of small (100-lb thrust) rocket motors using coaxial injection of hydrazine and nitrogen tetroxide
1961
27 S
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Numerical Study of Hydrazine and Nitrogen Tetroxide Combustion in small Rocket Motors
British Library Conference Proceedings | 1994
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