Aerodynamic Characteristics of a Model of an Escape Capsule for a Supersonic Bomber-Type Airplane at a Mach Number of 2.49

Author: Presnell, John G., Jr.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L57I17
Link: https://digital.library.unt.edu/ark:/67531/metadc63900/

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