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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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