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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

Language of Materials

From the Collection: Collection material is in English.

Access Information

The collection is open for research.

Extent

From the Series: 0.545 Cubic Feet (One letter-size full-width manuscript box and one letter-size half-width manuscript box)

Creator

Repository Details

Part of the Purdue University Archives and Special Collections Repository

Contact:
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