UAH Archives, Special Collections, and Digital Initiatives

Browse Items (8239 total)

  • Missgap_120407104405.pdf

    A thesis presented to the faculty of the Fletcher School of Law and Diplomacy. In partial fulfillment of the requirements for the Degree of Doctor of Philosophy.; This document is only the abstract of the thesis.; Document includes biographical note and table of contents.; aArchive copy is a photocopy.
  • Defense_Billboard_96_001.pdf

    People mourning someone at a funeral after that person decided to drink and drive
  • TheNASAGrumApol_052410121955.pdf

    Handwritten in pencil on the document. Describes the layout and function of various sections of the Apollo lunar module.
  • spc_mcca_000081-84_web.pdf

    The leaflet provides "Facts About The University of Alabama's New Huntsville Campus" including general information, student enrollments, and projected growth.
  • Potebiomappli_042209145355.pdf

    A brief history and purpose of nondestructive methods followed by a discussion of those methods.
  • Defense_Billboard_19_001.pdf

    Soldiers at war with American flag in the background
  • Defense_Billboard_93_001.pdf

    Soldiers at war with American flag in the background
  • theprooflartanforcryfue_071207131317.pdf

    Archive copy is a poor photocopy. Prepared for presentation at Deutsche Gesellschaft fur Raketentechnik und Raumfahrt. (German Society for Rocket Technology and Astronautics). Given by E. Harpoothian, Chief Engineer, Structures Department, Development Engineering.; Tanks for cryogenic fluids, as used in the Saturn space vehicles, have reached an advanced stage of design and development. Many of the structural features of the NASA/Douglas Saturn tanks, fabricated of 2014-T6 aluminum alloy, were first developed for the booster of the Thor ballistic missile, which later found extensive use in putting space vehicles into orbit. There is a mutual dependence of important factors related to design concepts, selection of materials, processing techniques, and fabrication methods. It is shown that this mutual dependence must be considered if a successful vehicle is to emerge from design and development. Details of vehicle structure, provision for insulation, and manufacturing methods are presented. Criteria for the selection of materials is shown to be dependent on strength, ductility, weldability, toughness, fabricability, behavior at cryogenic temperatures, and on manufacturing methods and inspection techniques.
  • thepromanpro_020408133725.pdf

    Included in "First Annual Logistics Management Symposium," Huntsville, Alabama; Archive copy is a poor photocopy. Describes the stages of rocket-development/launch and the logistical problems with each.
  • reliallupconc_070507141213.pdf

    Prepared for George C. Marshall Space Flight Center, Huntsville, Alabama under contract NAS8-11087. Publication No. 294-02-12-440. Special Technical Report No. 13.; INTRODUCTION: The Saturn/Apollo Systems Office at the George C. Marshall Space Flight Center (MSFC) requested ARINC Research Corporation to make a brief study of the reliability aspects of the All-Up concept. Under the requirements of Task 294-02 of Contract NAS8-11087, the study included a comparison between the reliability of the first Saturn V vehicle if All-Up, and its reliability with dummy upper stages.