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Theoretical Rocket Performance of Liquid Methane with Several Fluorine-oxygen Mixtures Assuming Frozen Composition

Sanford Gordon

出版	National Advisory Committee for Aeronautics, 1958
URL	http://books.google.com.hk/books?id=D7hFswEACAAJ&hl=&source=gbs_api

註釋

Theoretical rocket performance for frozen composition during expansion was calculated for liquid methane with several fluorine-oxygen mixtures for a range of pressure ratios and oxidant-fuel ratios.