UAH Archives, Special Collections, and Digital Initiatives

Browse Items (6320 total)

  • Nortamerrockjul1169_010711121426.pdf

    A news article detailing the scheduled launch for the Apollo 11. "Eagle" is the name of the lunar module and "Columbia" is the name of the service module.
  • commprobrelaluna_022807133241.pdf

    "This technical note concerns some of the problems encountered with the landing of a payload on the moon. The main problem areas such as guidance, velocity control and impact considerations are discussed. Although no final conclusions or designs are intended, it is hoped that the material presented will serve as a guide for future detailed work."
  • commbulkdraw.jpg.jpg

    8 x 10 inch black and white photograph; This is a cutaway drawing of the bulkhead with information about the LH2 tank skin, insulation, Aft LOX bulkhead, 2014-T6 alum skin and fiberglass core. Part of an envelope with photos accompanying C. E. Cataldo paper "Materials in Space Exploration."
  • freedomadober2_022607111422.pdf

    Includes bibliographical references.; Original format: paperback book (42 pages); Cover title: Resources for freedom : the outlook of energy resources, volume III. Contains plans and analyses of potential future energy sources.
  • comsysbladurreeoflarveh_031808114618.pdf

    This paper was published in the Proceedings of the IEEE, volume 55, number 5, May 1967.; ABSTRACT: Much of the theoretical research on reentry blackout is in a format difficult for the communications design engineer to use in his system analysis. This paper derives simplified equations for the average sheath power loss that may be added (in dB) to the usual space loss to obtain an approximate total propagation loss. The plasma and sheath properties are discussed in detail but largely without supporting mathematics, in order to give the design engineer a better understanding of the overall problem. For the same reason and to provide insight into the final results, the average radiated power is found, using both intuitive and rigorous techniques. Several graphs of plasma properties are included in the development as an aid to numerical computation, and results are compared with the work of other authors.
  • SkywSpacDiviVolXXIX17_052410122936.pdf

    A news article detailing the winners of scholarships from a competition held by Space Division. This contest was held for the children of Space Division employees.
  • compfaileffeonsystananalmode_062007111540.pdf

    Prepared by R. L. Parkhill, Section Chief, Saturn S-IVB Reliability Analysis and J. Pauperas JR., Asst. Section Chief, Saturn S-IV Reliability Analysis. Presented to the 4th Annual Seminar on Reliability for Space Vehicles, Los Angeles, California, December 6, 1963. This paper presents techniques originated by Douglas Engineering working under NASA contract NAS7-1. Prepared as a record of the study conducted for the Administrative Engineer on the Department Overhead Account No. 9703.; SUMMARY: In today's complex systems, such as Saturn, many traditional reliability analysis concepts are not acceptable. Because of time and budget restrictions, and the requirement to provide a "man rated" space vehicle, the Douglas Saturn Engineering Reliability Section has developed a new analytical approach; it is called "criticality ranking". It is a "totem pole" of components whose single failure may lead to system loss. "Criticality ranking" is one of the results of an analytical model which encompasses failure effect and reliability prediction. This paper describes this analytical model, discusses some of the techniques and ground rules, and presents examples. A discussion of the application of the results is also included.
  • Compcontpowe_042908131740.pdf

    This paper describes a real-time digital computer program that controls the application of electrical power to the S-IVB stage of the Saturn vehicle at Cape Kennedy, Florida. Douglas Aircraft Company, the S-IVB stage manufacturer, provided NASA with the program requirements relative to the energizing sequence, voltage and current measurement tolerances, and vehicle system operational tests. International Business Machines Corporation provided NASA with the computer program to satisfy the task requirements. The program conjoined the components of the Electrical Support Equipment (two RCA 110A computers and control and instrumentation devices) into a closed loop system. The supporting operating system program by IBM is described.
  • Computerredundancy_020608095718.pdf

    Discusses the importance of redundancy as a safety measure in electronic systems.
  • conditions.jpg.jpg

    8 x 10 inch black and white photograph. A photograph of a list of things contributing to stress corrosion. Referenced by "Materials in Space Exploration." Is part of envelope containing photos accompanying C. E. Cataldo paper "Materials in Space Exploration."
  • 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.
  • 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
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