Box 2
Container
Contains 1 Collection or Record:
Rieble, G. D.; Small, W. J.; Morris, O. A. Aerodynamic Tests and Analysis of a Turbojet-Boosted Launch Vehicle Concept (Spacejet) Over a Mach Number Range of 1.50 to 2.86. NASA Technical Paper 1888. NASA Technical Memorandum 81963. NASA Scientific and Technical Information Branch, July 1981
Item — Box: 2, Item: 19
Identifier: MSA 312, Series 2, Item 19
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:
July 1981