UAH Archives, Special Collections, and Digital Initiatives

Browse Items (7888 total)

  • loc_burw_-95.pdf

    The conductor's report notes 158 passengers in coach from Augusta to Atlanta.
  • Confmana_071907091418.pdf

    Configuration management: Definition, requirements, organization, policy and procedure documents, contractual documents.
  • spc_mcca_000143-151.pdf
  • contrstatrpt_062807110849.pdf

    Saturn funded contracts in excess of $100,000. Lists contracts by contract numbers. Gives contractor, value, place of performance and scope of work.; There is a burned stripe across one page.
  • Contprogprocedure_090308135708.pdf

    Outlines various procedures for Saturn V contractors.
  • contprogproc_101007154101.pdf

    A collection of various procedures. Archive copy is a photocopy. There is no continuous numbering in this document.
  • ContpricsatuSII_120408111902.pdf

    Indicates the various levels and responsibilities within the Saturn V pricing and contract personnel. September 3, 1968.; Approved S. L. Weinberg.
  • Contrforsatuuppe_120108134449.pdf

    Details contracts for upper stages of Saturn IV and Saturn V and includes illustrative appendixes. Archive copy is a photocopy.
  • Defense_Billboard_49_001.pdf

    Uses doll, chick and fox to convey inappropriate terms for addressing women
  • corrprobasswithspaclaunveh_031607135408.pdf

    A document reporting various space vehicle corrosion issues. Original is photocopy.
  • corrprobasso.pdf.pdf

    Corrosion problems associated with space vehicles, in general, are discussed as contrasted to those problems experienced with structures in an earth atmosphere. Primary emphasis is placed on structural alloys in this discussion, although some corrosion failures experienced in various mechanical components are described. General corrosion prevention measures are indicated, and solutions to specific corrosion failures described. Major failures experienced have been attributed to stress corrosion cracking, rather than general or galvanic type corrosion. Most such failures have occurred with only five different materials: three aluminum alloys - 7075-T6, 7079-T6, and 2024-T6; and two precipitation hardening stainless steels - 17-7PH and AM 355. Corrective actions were different in each case, but involved either a complete change to another material, a change to a different temper of the same alloy, or a modification of the heat treatment and/or general processing techniques. General conclusions are that the types of failures described could be avoided by: a more suitable selection of alloys in the initial design, a realistic review of the environments that could be encountered in the service lifetime of the component, lowering stresses, improving process controls, and effecting better familiarization of design personnel with the with the overall stress corrosion problem in an effort to reduce human error.; Preprint 18e.; Materials for re-entry and spacecraft systems - spacecraft materials.; Materials Conference, Philadelphia, Pennsylvania, March 31 - April 4, 1968.
  • loc_mshc_0000024_web.pdf

    The photo shows the north side of courthouse square looking east in downtown Huntsville. The Madison County Courthouse can be seen at the right of the photo.
  • counlift_080607123539.pdf

    This is an article from the Boeing Magazine. The Archive copy is a very poor photocopy and is difficult to read.; About the time the S-IC-1 booster is lifting the first Apollo/Saturn V from the launch pad on its maiden unmanned flight next year, a Boeing systems test crew will begin static testing the S-IC-4 at Devils Swamp, Mississippi (MTF). Starting with S-IC-4, all Saturn V first stage boosters will be captive fired at MTF. At present, S-IC firings are conducted by MSFC's test laboratory at Huntsville. The first flight stage, the S-IC-1, was placed in the static test stand on 24 January 1966 and completed its test program 25 Feb. It was removed from the stand March 14 and is undergoing post-firing checkout. it is due to be shipped this summer to KSC where it will be mated to the two upper stages of Saturn V, the IU and Dummy Apollo payload. The S-IC-2 went into the static stand on March 22 and is being tested during April The S-IC-3 also will be tested at Huntsville in 1966. The job of putting the world's largest and most powerful rocket together will be accomplished in the world's largest building, the 52-story vehicle assembly building.
  • Skywritdec668_032210105145.pdf

    News article detailing how the crew of the Apollo 8 are preparing for launch with a "dry run."
  • Skywritjan2469_031510153022.pdf

    News article detailing how the Apollo spacecraft 107 command modules are planned to be used in future space-missions.
  • Crewbrieinst_012309113213.pdf

    Document outlining different slides of a presentation containing numerous organizational charts, diagrams and bullet-list points.
  • Crewbrieinst_012709172107.pdf

    Document outlining different slides of a presentation containing numerous organizational charts, diagrams and bullet-list points.
  • loc_salm_000275_000277.pdf

    The book includes details about Salmon's exchange transactions while stationed in Europe in spring 1946.
  • spc_mcca_000005_web.pdf

    This is a typed list of the journal subscriptions for the library in 1962-1963 with additional journals written at the bottom of the list. At the top of the document, there is a written note to "Dr. Roberts," presumably history professor Frances Roberts, requesting she renew all of the subscriptions.
  • d5-13197.pdf.pdf

    This Manufacturing plan is prepared in response to the Apollo Applications Program request for proposal No. 1.1.; PURPOSE: The purpose of this document is to present a Boeing plan for the manufacturing effort required to provide hardware and support for the installation and checkout of Experiment Packages and related equipment in the Apollo Systems Modules.
  • http://dkdayton.net/roberts/images/r01b/pdfs/r01b23-12.pdf

    March 16 1872
  • Defense_Billboard_30_001.pdf

    Different branches of the military on their off time getting into danger
  • J2rockengidata_120408110834.pdf

    A datasheet describing the function of the J-2 rocket engine.
  • H1rocengdatsht_090408145504.pdf

    News from Rocketdyne.
  • spc_dann_000254.mp4

    The Dannenbergs travel down to Daytona Beach, Florida, to see the launch of Apollo 15. The first half shows the resort and Ingeborg sitting by the beach. The second half shows the drive to the launch facility in Cape Canaveral, Florida and the traffic they find upon arrival. 1971.
  • spc_dann_000219.mp4

    Konrad, Klaus, Ingeborg, and Betty Dannenberg and little George vacation with the Ullrichs (Rita and Hanns) in Daytona Beach, Florida. They are all shown playing on the beach outside of their resort. 1967.
  • spc_dann_000216.mp4

    Ingeborg, Konrad, Klaus, and Betty Dannenberg and little George relax by the pool at their resort in Daytona Beach, Florida. The video focuses mostly on George playing with a toy boat both in and out of the pool. 1967.
  • img_00057.pdf

    Front: "De Lan' O' Cotton."
  • SkywritDec2068_032210104848.pdf

    News article detailing how Apollo 8 is ready for launch and the anticipation surrounding it.
  • Deciprocforminicost_100107112756.pdf

    Prior to acceptance of a liquid rocket engine for use in Saturn vehicles, the average thrust of two consecutive tests without an intervening calibration must satisfy specification requirements. The contractor may recalibrate after the first and subsequent tests if he so chooses, based upon decision limits, until the above requirement is met.
  • Defense_Billboard_70_001.pdf
  • Defense_Billboard_110_001.pdf

    Various pictures of women in the Armed Forces throughout history
  • spc_dann_000184.mp4

    Trip to Frankfurt, West Germany. Shows multiple shots of Frankfurt airport as well as taking off and aerial views of Germany. Final shots show touchdown in New York and the reception area inside of a New York airport. "Ffm" is an abbreviation of Frankfurt am Main. 1960.
  • desidevel1500pounthru_062507103113.pdf

    Describes the F-1 engine design and components.
  • desdevzerogvapliq_071207111927.pdf

    During long coast periods of zero-gravity, storage vessels for the cryogenic liquids proposed for use in some power transmission systems undergo random distribution of the liquid and vapor phases therein. Thus, when heat flow into the vessel causes the vessel pressure to build-up requiring venting to maintain a safe value, the likelihood of venting the valuable liquid phase, as well as the vapor, results. To preclude this eventuality, various devices for separating the liquid and vapor phases and venting just the vapor have been studied and carried into the experimentation stages.
  • Desiusefaulsimu_110107110239.pdf

    Describes different aspect of the Fault Simulation for Saturn computer design.
  • desconofgroddasinsat1BVESE_020108113351.pdf

    In the Saturn IB/V programs the sheer quantity of data required for computer processing and ESE display makes it necessary to provide an efficient data acquisition system. For much of the data originating in the launcher this requirement is satisfied by the Ground Digital Data Acquisition System (DDAS). This paper provides a technical description of the Ground DDAS with emphasis placed on the unique design concepts of this telemetry system.
  • desiofthesatus-ivstagproputilsyst_041307164422.pdf

    Describes the SIV vehicle and its components. Presented at: IRE International Convention.
  • desdevfabric_071107111534.pdf

    For presentation to the Society of Automotive Engineers, 16 September 1964, Boston, Massachusetts. ABSTRACT: This paper discusses the design, development and fabrication of a prototype hydraulic transformer, Hydro-Aire Model No. 05-055, performed in fulfillment of the requirements of Contract No. NAS 8-5264 for NASA Marshall Space Flight Center. The Hydraulic Transformer described is designed to pump hydraulic oil at a flow of 100 GPM with a pressure rise of 4000 psi, and does this work by utilizing as a power source the flow of RP-1 rocket fuel at a pressure of 1900 psig. The Hydraulic Transformer built to handle this combination of flows and pressures, unprecedented in such devices, has a weight of only 70 pounds for the first development model. The development of this unit is discussed and future development improvements are mentioned.
  • devandutiofcomtesproforcheofspaveh_110907133554.pdf

    A computer system was designed to allow test engineers to progressively employ automation in the checkout of the Uprated Saturn I and Saturn V space vehicle programs and still allow manual control of the checkout process. A two-computer system was selected by National Aeronautics and Space Administration, and the International Business Machines Corporation was chosen to provide the programming engineering necessary to implement these objectives. Space vehicle checkout, prior to launch, may be characterized by controlling, monitoring, and testing the vehicle and its subsystems through the use of ground support equipment (GSE).; IBM Huntsville Library.; Presented at AIAA Conference, XVIIth International Astronautical Congress, Madrid, Spain, October 10-15, 1966 by Edward A. Robin, Manager, Vehicle Test Programming Department.
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