Combustion Characteristics of a Swirling LOX Type Hybrid Rocket Engine
نویسندگان
چکیده
منابع مشابه
Parametric Trends in the Combustion Stability Characteristics of a Single - Element Gas - Gas Rocket Engine
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ژورنال
عنوان ژورنال: JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
سال: 2006
ISSN: 1344-6460
DOI: 10.2322/jjsass.54.242