Box 2
Container
Contains 1 Collection or Record:
Pittman, J. L.; Riebe, G. D. Experimental and Theoretical Aerodynamic Characteristics of Two Hypersonic Cruise Aircraft Concepts at Mach Numbers of 2.96, 3.96, and 4.63. NASA TP-1767, NASA Scientific and Technical Information Branch, December 1980
Item — Box: 2, Item: 17
Identifier: MSA 312, Series 2, Item 17
Scope and Contents
From the Series:
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Dates:
December 1980