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Box 2

 Container

Contains 27 Collections and/or Records:

Printed Material, 1953 - 1986

 Series — Multiple Containers
Identifier: MSA 312, Series 2
Scope and Contents 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: 1953 - 1986

National Advisory Committee for Aeronautics, Ames Research Center. Equations, Tables, and Charts for Compressible Flow. Washington, DC: Government Printing Office, 1953

 Item — Box: 2, Item: 1
Identifier: MSA 312, Series 2, Item 1
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: 1953

Schaefer, W. T. Jr. Characteristics of Major Active Wind Tunnels at the Langley Research Center. NASA TM X-1130. Washington, DC: National Aeronautics and Space Administration, 1965

 Item — Box: 2, Item: 2
Identifier: MSA 312, Series 2, Item 2
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: 1965

Historical Aspects of NASA Scramjet Technology Development, by E. A. Mackley, circa early 1970s

 Item — Box: 2, Item: 3
Identifier: MSA 312, Series 2, Item 3
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: circa early 1970s

Hypersonic Research Facilities Study, Volume I, Summary, prepared under Contract No. NAS2-5458 by Advanced Engineering at McDonnell Aircraft Company for OART – Advanced Concepts and Missions Division, NASA, Moffett Field, California, October 1970

 Item — Box: 2, Item: 4
Identifier: MSA 312, Series 2, Item 4
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: October 1970

Hunt, J. L.; Talcott, N. A. Jr.; Cubbage, J. M. Scramjet Exhaust Simulation Technique for Hypersonic Aircraft Nozzle Design and Aerodynamic Tests. Hampton, Virginia: NASA Langley Research Center, 1977

 Item — Box: 2, Item: 5
Identifier: MSA 312, Series 2, Item 5
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: 1977

Talcott, N. A. Jr. Thermodynamic Properties of Gaseous Fluorocarbons and Isentropic Equilibrium Expansions on Two Binary Mixtures of Fluorocarbons and Argon. NASA TN D-8405. Washington, DC: National Aeronautics and Space Administration, 1977

 Item — Box: 2, Item: 6
Identifier: MSA 312, Series 2, Item 6
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: 1977

Draper, A. C.; Lane, P. Jr.; Zima, W. P. A Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology. Wright-Patterson Air Force Base, OH: Air Force Flight Dynamics Laboratory. (printed in AIAA 1977 AFM Conference, August 8 - 10, 1977

 Item — Box: 2, Item: 7
Identifier: MSA 312, Series 2, Item 7
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: August 8 - 10, 1977

Talcott, N. A. Jr.; Hunt, J. L. Streamtube Analysis of a Hydrogen-Burning Scramjet Exhaust and Simulation Technique. Reprinted from Journal of Aircraft, Vol. 14, No. 9, September 1977, pp. 918-920, September 1977

 Item — Box: 2, Item: 8
Identifier: MSA 312, Series 2, Item 8
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: September 1977

Talcott, N. A. Jr.; Hunt, J. L. Calculated Heating on the Afterbody Nozzle of a Hypersonic Aircraft Concept. Reprinted from Journal of Aircraft, Vol. 14, No. 12, December 1977, pp. 1247-1248, September 1977

 Item — Box: 2, Item: 9
Identifier: MSA 312, Series 2, Item 9
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: September 1977

Talcott, N. A. Jr. Flow Field Visualization About External Axial Corners. NASA TM-78682. Hampton, Virginia: NASA Langley Research Center, 1978

 Item — Box: 2, Item: 10
Identifier: MSA 312, Series 2, Item 10
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: 1978

Weidner, J. P. The Application of Dual Fuel (JP-LH2) for Hypersonic Cruise Vehicles. Reprinted from Journal of Aircraft, Vol. 15, October, pp. 686-691, 1978

 Item — Box: 2, Item: 11
Identifier: MSA 312, Series 2, Item 11
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: 1978

Weidner, J. P. Conceptual Study of a Turbojet/Ramjet Inlet. NASA TM-80141. NASA Scientific and Technical Branch, 1979

 Item — Box: 2, Item: 12
Identifier: MSA 312, Series 2, Item 12
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: 1979

Beach, H. L. Jr. Hypersonic Propulsion, NASA Conference Publication 2092, Aeropropulsion 1979, Proceedings of a Conference held at NASA Lewis Research Center, Cleveland, Ohio, May 15 - 16, 1979

 Item — Box: 2, Item: 13
Identifier: MSA 312, Series 2, Item 13
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: May 15 - 16, 1979

Small, W. J.; Riebe, G. D.; Taylor, A. H. Aerodynamics of a Turbojet-Boosted Launch Vehicle Concept, presented at the AIAA 18th Aerospace Science Meeting, Pasadena, CA, January 14 - 16, 1980

 Item — Box: 2, Item: 14
Identifier: MSA 312, Series 2, Item 14
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: January 14 - 16, 1980

Weidner, J. P. Propulsions/Airframe Integration Considerations for High Altitude Hypersonic Cruise Vehicles, presented at the AIAA 18th Aerospace Sciences Meeting, Pasadena, CA, January 14 - 16, 1980

 Item — Box: 2, Item: 15
Identifier: MSA 312, Series 2, Item 15
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: January 14 - 16, 1980

Vahl, W. A.; Weidner, J. P. A Preliminary Assessment of the Impact of 2-D Exhaust-Nozzle Geometry on the Cruise Range of a Hypersonic Aircraft With Top-Mounted Ramjet Propulsion. NASA TM -81841. NASA Scientific and Technical Information Branch, 1980

 Item — Box: 2, Item: 16
Identifier: MSA 312, Series 2, Item 16
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: 1980

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

Talcott, N. A. Jr. The Use of Interactive Graphic Displays for Interpretation of Surface Design Parameters. NASA Technical Memorandum 81963. NASA Scientific and Technical Information Branch, May 1981

 Item — Box: 2, Item: 18
Identifier: MSA 312, Series 2, Item 18
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: May 1981

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

Heldenfels, R. R. Some Historical Perspectives on Thermostructural Research at the NACA Langley Aeronautical Laboratory, 1948-1958, presented at Symposium on Computational Aspects of Heat Transfer in Structures, Langley Research Center, Hampton, Virginia, November 3 - 5, 1981

 Item — Box: 2, Item: 20
Identifier: MSA 312, Series 2, Item 20
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: November 3 - 5, 1981

Talcott, N. A. Jr. Computer Graphics Display Technique for the Examination of Aircraft Design Data. Reprinted from Journal of Aircraft, Volume 19, Number 1, pp. 76-80, January 1982

 Item — Box: 2, Item: 21
Identifier: MSA 312, Series 2, Item 21
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: January 1982

Hunt, J. L.; Johnston, P. J.; Cubbage, J. M., et. al. Hypersonic Airbreathing Missile Concepts Under Study at NASA Langley Research Center. AIAA 20th Aerospace Sciences Meeting, Orlando, Florida, January 11 - 14, 1982

 Item — Box: 2, Item: 22
Identifier: MSA 312, Series 2, Item 22
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: January 11 - 14, 1982

Wieting, A. R. Modification of 8 Foot High Temperature Tunnel to Provide a Unique National Research Facility for Hypersonic Air-Breathing Propulsion Systems, Proposed LaRC FY 85 CoF, September 1982

 Item — Box: 2, Item: 23
Identifier: MSA 312, Series 2, Item 23
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: September 1982

Material and Structural Aspects of Lifting Re-Entry Aerospace Flight Systems, PowerPoint presentation sheets, no author, circa 1982

 Item — Box: 2, Item: 24
Identifier: MSA 312, Series 2, Item 24
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: circa 1982