UAH Archives, Special Collections, and Digital Initiatives

Browse Items (7888 total)

  • Defense_Billboard_50_001.pdf

    A man and woman's shoes on the floor with rain on the floor and the shoes
  • loc_mshc_0000031_web.pdf
  • thehisofarmmisdev_121707120332.pdf

    Published as "Army Missile Development," Army Information Digest, XI. Establishes the development and history of weaponized rocket ordenance.
  • http://dkdayton.net/roberts/images/r10/pdfs/r10_03-14.pdf
  • http://dkdayton.net/roberts/images/r04a/pdfs/r04a03-27.pdf
  • IBMcleanroomcome_042209102226.pdf

    A history of the IBM's Space Systems Center clean room and a description of its uses.
  • Impamanudesi.pdf

    The purpose of this paper is to emphasize the need for accessibility in the assembly and maintenance of spacecraft. This is especially pertinent because accessibility to subsystems for replacement, repair, and maintenance has proven to be one of the more costly phases of preflight preparation. The most successful programs in this day and age have been when the design and manufacturing engineers work side by side around a mockup where solutions to the problems can be visually seen and solved, keeping in mind the assembly as related to accessibility. Therefore, it will be shown that in order to overcome the difficulties, designers should adapt a hard, fast ground rule that each unit must be accessible and individually removable without disturbing the other units.; Aeronautic and Space Engineering and Manufacturing Meeting, Los Angeles, Calif. Oct. 7 - 11, 1968.
  • InflapolsatuV_061908163151.pdf

    This paper presents some relationships between Apollo/Saturn V launch operations and multiple lunar landing sites, including the means by which site selection could facilitate launch operations.
  • insspaveh.pdf

    Presented on September 21, 1962, at the Eleventh Tagung Der Deutchen Raketen - Gesellschaft, Koblenz, West Germany. Instrumentation sf the Saturn space vehicle represents a considerable effort during the development phase, for proper design evaluatian of this new configuration, its propulsion system, and its structure and control characteristics, an unprecedented number of measurements are required to be carried onboard and to be recovered, These measurements are expected to work properly and to furnish the design engineer with information that is not available by ground testing,
  • Iterguidlawsatu_080707154609.pdf

    Summary: "Based on Lawden's equation, semi-explicit,'iterative' Saturn guidance equations are derived, many were successfully flight tested on Saturn I and analyzed for the main Apollo mission and other applications applications."
  • j2liqhydrrock_060607141431.pdf

    The 5-2 high-energy liquid propellant rocket engine (~i~. l), a large engine producing 200,000 pounds of thrust at altitude conditions, burns liquid hydrogen and liquid oxygen to produce the necessary high specific impulse for practical space use. Rocketdyne, a Division of North American Aviation, Inc., is developing the engine for the George C. Marshall Space Flight Center, Xfi. The first use of the engine will be in the upper stages of the Saturn vehicles. Five engines will be used for the second, S-I1 stage of the Saturn V, and one will power the S-IVB third stage of the Saturn V and S-ISTI second stage of 'the Saturn IB; Original is a photocopy on onion skin.
  • loc_hutc_518_524.pdf

    Reprinted as part of the Alabama sesquicentennial celebration, this pamphlet was originally produced for the dedicated of the new Madison County Courthouse in 1967. Includes an order form for a special sesquicentennial edition of Valley Leaves.
  • Defense_Billboard_137_001.pdf
  • 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.
  • relipictmsfcphilstaffmgmt_031907142349.pdf
  • Theroleofsimuinthedeveofanautochecsyst_110507111856.pdf

    For publication in Luftfahrttechnik Raumfahrttechnik. Discusses the uses and advantages to using simulations.
  • rolenasamsfcmanufeng_071207105624.pdf

    For presentation at the Aerospace Industries Association of America (AIA) Manufacturing Engineering Committee Meeting. Discusses the role the NASA Engineering Laboratory has had on NASA projects in the form of vehicles and smaller projects.
  • Roles-ivbapol_041508165617.pdf

    Douglas Paper No. 4396.; Prepared by Ludwig Roth, Director, Saturn/Apollo Program Extension, Douglas Aircraft Company.; Presented to 16th Annual Conference of the Hermann Oberth Society. Discusses the role of the Apollo rocket after the Apollo program has concluded.
  • Roleweigdevefiri_090607095535.pdf

    Speech regarding the importance of developing and upgrading space ships and space technology.
  • satiblauvehsyst_071107131340.pdf

    Speech containing information regarding Crystler's role in the Saturn Project as contracted builders of the stages of three space vehicles.
  • Satulaunvehifami_091707161639.pdf

    Presentation focusing on the history of Saturn V's engineering history and crew.
  • Satulaunvehi_081407123504.pdf

    General O'Connor's presentation to the American Institute of Aeronautics and Astronautics. Centers around saturn space vehicles and makes references to slides.
  • saturnsii_062907104459.pdf

    The S-II is the second stage of NASA's Apollo moon-landing rocket - the giant Saturn V. The most powerful hydrogen-fueled booster under production, the S-II is destined for Apollo manned lunar missions and will help power three Americans to the moon. The S-II is being developed and manufactured at Seal Beach, Calif., by North American's Space and Information Systems Division, Downey, Calif., under the technical direction of NASA's Marshall Space Flight Center, Huntsville, Ala.
  • Satuvmissalab_080707155420.pdf

    Speech that covers the topics of the Saturn V lunar mission and the basics of a lunar mission in general.
  • loc_salm_000313_000315.pdf

    This greeting card was sent from M. Louis Salmon in Vienna, Austria to his parents in Mobile, Alabama at Christmas 1945. The inscription reads, "Your devoted son, Louis."
  • sigparamaffheat_071907135246.pdf

    The Saturn S-IVB stage has a requirement for orbiting around the earth for up to 4.5 hours with approximately 60 percent of its initial propellant remaining at the end of the coast (prior to restart) . Extensive analyses must be performed to insure that this requirement is met. Both the maximum and minimum heat transfer rates are important because the maximum rates affect the hydrogen boiloff losses and thus the initial propellant loading requirements. The minimum rates are important because the boil off gases are used to maintain a minimum axial thrust level by venting the gases continuously through aft facing nozzles. This provides for a settling of the propellant throughout the orbital coast and alleviates the need for periodically venting the tank under zero gravity.
  • sdsp_skyl_000090_001.pdf

    Students involved in the student experiment selection are: Bochsler, Daniel C., Converse, Vincent W., Crites, Troy A., Dunlap, W. Brian, Hamilton, John C., Hopfield, Alison, Jackson, Kathy L., Johnston, Roger G., Leventhal, Jeanne L., Meister, Todd A., Miles, Judith S., Peltz, Cheryl A., Quist, Terry C., Reihs, Joe W., Schlack, Donald W., Wordekemper, Joel G., Shannon, Neal W., Staehle, Robert L., Zmolek, Joe B. Students whose experiments were held in consideration for future programs are Stein, Keith L., Brandt, Kent M., McGee, Keith, Sherhart, Kirk M., Merkel, Gregory A., Healy, James E.
  • img_01203.pdf

    Front: The State Agricultural and Mechanical College for Negroes, Huntsville, Ala.
  • spc_dann_000127.mp4

    Konrad, Ingeborg, and Klaus Dannenberg see Teton National Park and Yellowstone National Park. In Yellowstone, Konrad captured footage of the "mud volcano" and the "dragon's mouth" as well as some local wildlife. Summer 1956.
  • Thetoughestweldofall_061908141303.pdf

    Article explores the outer layer of the Saturn S-II along side its benefits and complications. Contains poorly rendered images displaying the process.
  • spc_spac_000306_000309.pdf

    This leaflet contains photographs, descriptions, and specifications of the Trackless/Train.
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