UAH Archives, Special Collections, and Digital Initiatives

Browse Items (970 total)

  • newsrocketdyne_062907104301.pdf

    Press release exploring the rockets and projects of the Saturn project.
  • newsreleaseliqhydrog_041207113432.pdf

    Press release covering the nature and use of liquid hydrogen
  • nextstopthemoon_030209161111.pdf

    Release describing the launch of the Apollo 11.
  • Nexuconc.pdf

    Aspects of Earth-to-orbit delivery are discussed and a cost analysis of the logistic operation and the cost of orbital operations are presented. Probabilities of success of orbital delivery and the operational and economic aspects of establishing large orbital installations and maintaining a large transportation volume in the 1975/85 time period are compared for the two cases using a large number of Saturn V versus a smaller number of 1-stage chemical Post-Saturn launch vehicles. Performance parameters of chemical, chemonuclear and nuclear launch vehicles are compared. The concept of a blunt launch vehicle configuration referred to as NEXUS is presented in detail. Applications of this configuration to chemonuclear propulsion and to a 50 ft diameter version of Saturn V with recoverable first stage are discussed.
  • NoisReduStudScalModeAcouTestFaci_072508164059.pdf

    The acoustic properties of five insulation materials were investigated in a 1/10- scale model acoustic facility. The materials were designed for applications in space vehicles. The model facility, consisting of a reverberation chamber coupled to an anechoic chamber, was evaluated for its use in noise reduction testing. It was found that a reasonably diffuse sound field existed above 900 Hertz. Modal density graphs of the reverberation chamber and spatial acoustic gradients measured within the chamber and across the test panel opening are compared to an idealized facility.; Prepared for the 75th Meeting of the Acoustical Society of America,Ottawa, Ontario, Canada. May 21 - 24, 1968.
  • NondesTest_021508092714.pdf

    Presented at the Western Metals Congress, Los Angeles, California, 15 March 1967.; Archive copy is a photocopy.; ABSTRACT: This report describes the various nondestructive test methods employed to evaluate materials and processes used in the manufacture of large liquid propellant rocket engines at the Rocketdyne Division of North American Aviation, Inc. The contents of the paper were purposely oriented for an audience of aerospace, design and materials engineers. A brief description of liquid propellant rocket engine reliability is presented. The relationship of standards and specifications to nondestructive testing is discussed and various test methods are described along with a discussion of their applications and limitations. The sequence of events leading up to the use of nondestructive testing in production inspection is presented. Finally, the organization of labor directly related to nondestructive testing is given.
  • Nortamerrockoct369_082111193015.pdf

    An entire newspaper containing a number of articles both related and not related to the Saturn program.
  • norhunorgchanorcororgcha_051608135828.pdf

    Nortronics/Northrop corporate organizational chart. Contains descriptions of the staff below the charts.
  • Notetodrmuelfromsamu_120208111242.pdf

    a note to Dr. Mueller from Samuel C. Phillips regarding the designations of space vehicles.
  • slywritersd_041910103841.pdf

    A news article detailing a Technology Exchange event held by North American Rockwell Corperation.