Description: Report presenting performance estimates for a family of airplanes designed to cruise at Mach number 4.25 and using General Electric AC-210 ramjet engines. The airplane was designed to carry a payload of 10,000 pounds and use a crew of one. Results regarding the shield weight, engine weight, number of engines, and nozzle-velocity coefficient are provided.
Date: April 11, 1958
Creator: Weber, Richard J. & Connolley, Donald J.
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Partner: UNT Libraries Government Documents Department