Screaming tendency of the gaseous-hydrogen - liquid-oxygen propellant combination
Description:
Report presenting an exploratory study of the screaming tendency of the gaseous-hydrogen-liquid-oxygen propellant combination in 200-pound-thrust rocket engines. Four injector classes in a total of 12 different configurations were tested in a variety of chamber lengths over the usable mixture-ratio range. Results regarding acoustic oscillations, unclassified oscillations, driving and damping mechanisms, and effects of screaming on heat transfer are provided.
Date:
September 30, 1958
Creator:
Baker, Louis, Jr. & Steffen, Fred W.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department