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Scramjet Test Facility Operational Envelopes

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Facility Altitude vs. Mach# Envelopes

Please note: These test envelopes have been contructed using an assumed forebody precompression and inviscid oblique shock theory to relate facility nozzle exit conditions to flight. Actual simulated flight conditions will vary depending upon test article design and installation details

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Last updated: Thursday, August 14, 2008 14:48