UAH Archives, Special Collections, and Digital Initiatives

Browse Items (7888 total)

  • spc_stnv_000029.pdf

    This document is a compilation of abstracts of NASA Technical Memorandums and MSFC Internal Notes, written by personnel of the Materials Division and released during 1965.
  • spc_mcca_000223-224.pdf

    The program includes the banquet menu, the program events, and a list of SGA officers and legislators.
  • loc_burw_film_009.mp4

    Home movies of the Burwell family as they settled into their new home in Huntsville. There is some vacation footage but the majority of the film is of mid-century Huntsville and Chattanooga.
    Beach scenes [11:55]
    Cattle and rural scenes [09:57]
    Chores [08:02]
    Clay shooting [09:13]
    Dog [00:01, 4:38, 7:46, 18:01, 20:01, 20:51]
    Fly [21:33]
    Homes [02:28, 03:10]
    Snow [03:52, 06:46]
    Lookout Mountain Hotel [09:07]
  • spc_dann_000239.mp4

    Ingeborg and Konrad Dannenberg visit their friends the DeBeeks in Webb City, Missouri. The first part of the film shows them sightseeing on main street, and the second half contains their visit with the DeBeeks. 1969.
  • spc_dann_000280.mp4

    Film shows Kerry, Klaus, Christie, and Betty Dannenberg ice skating at a public rink in 1976. Location unknown.
  • loc_burw_film_012.mp4

    Home movies that primarily depict a Christmas scene and an extended cruise around the Caribbean.
    Christmas [00:02]
    Royal Caribbean Resort in Labadie, Haiti [05:03]
    Punta Cana, Dominican Republic [08:16]
    Miami [09:44]
  • loc_burw_film_020.mp4

    The label on the inside of the can notes, "B&W Jeff horse back riding. Picnic with Dave 1951. Christmas 1950."

  • spc_dann_000232.mp4

    Film shows Kerry crawling and walking in the Dannenbergs' yard alongside Ingeborg and Lucky. Monte Sano, Huntsville, Alabama. Konrad Dannenberg's note on the film box reads, "2 Sept 1968 - (Klaus and Betty are in Acapulco, (Mex) / Kerry, IMK & Lucky at home - Ks first steps / first in Backyard then - frontyard / K winds up crying!" Fall 1968.
  • spc_dann_000230.mp4

    Video shows Kerry Dannenberg crawling around the Dannenbergs' backyard, with appearances by Lucky, Klaus, and Betty Dannenberg. Konrad Dannenberg's note on the front of the film box reads, "First attempts to walk / but he keeps on crawling." On the reverse, his note reads: "25 Aug 1968 - Kerry in Backyard / 5130 Panorama / also w/Lucky crawling on lawn / crawling up/down steps." Summer 1968.
  • spc_dann_000169.mp4

    This film shows the starting work on the Dannenbergs' new house. They first chop down and burn all of the foliage that's growing where the house will be. Then a construction crew comes in and grades the site. The final shot shows Konrad and Klaus Dannenberg marking the corners of the new house. Konrad Dannenberg's notes on the film box read, "1) Cleaning of House Area, Tommy + Klaus 2) Grading w/ Digger (IMK) 3) Woodburning + chopping 4) [illegible] and hose w/ transit 5)Ko and Klaus setting up corners. Very good film!" Summer 1958.
  • spc_dann_000201.mp4

    Konrad, Klaus, and Ingeborg Dannenberg open presents with company over during Christmas at the Dannenbergs' house in Monte Sano, Huntsville, Alabama. Konrad Dannenberg's notes on the film box read, "Unwrap gifts [illegible] ... Ulla, George, Erna, Alma, Kl, IMK + Ko Under X mas tree." Winter 1963.
  • spc_dann_000138.mp4

    (Originally titled "X-mas 1956" and dated as such.) Film shows new construction on Panorama Drive in Huntsville, Alabama. Dannenberg family members Konrad, Klaus, and Ingeborg as well as their new dog walk around the site and help out the construction workers. Konrad Dannenberg's notes on the side of the film box read, "1) The 'Batterboards' are up 2) Laying of Concrete Blocks 3) IMK w/Peabody - Ulla w/Peabody 4) Klaus and Ko filling in Foundation 5) Life Size Shot of Ko w/hatchet." Winter 1958.
  • spc_dann_000269.mp4

    The first half of the film shows Konrad Dannenberg surveying the stands for spectators of Apollo 16 at the launch complex in Cape Canaveral, Florida. The second half of the film follows the rocket as it lifts off from the launch pad and ascends out of view. Spring 1972.
  • zerostage_082707085507.pdf

    To meet the demands of increasing payload size and weight, and to fill the large payload gap between the Saturn IB and Saturn V, a number of methods of uprating the Saturn IB have been studied by NASA and Chrysler Corp. of providing increased payload capability is discussed in this paper. Four 120 in. United Technology Center UA-1205 solid propellant motors, originally developed for the Air Force Titan III program, are clustered around the S-IB first stage of the Saturn IB launch vehicle. These four solid propellant motors provide the total thrust for liftoff of the vehicle, with S-IB stage ignition occurring just prior to burn-out and separation of the solid propellant motors. The term "Zero Stage" is applied to this added stage.
  • spc_stnv_000030.pdf
  • spc_stnv_000142.pdf

    This official bibliography includes English- and foreign-language books, articles, and interviews.
  • spc_stnv_000139.pdf

    The document is designated for internal use only.
  • comparadvcoolingtech_071207135801.pdf

    The document is a technical paper for Astronautics and Aerospace Engineering Magazine.The copy has handwritten notes that appear to be for revisions. The abstract states "In the early days of rocket propulsion, two primary methods were employed for cooling the walls of thrust chambers. These were uncooled metal chambers where the heat sink capacity of the chamber and nozzle wall materials limited the operating duration, and regeneratively cooled chambers where one of the propellants was circulated in a cooling jacket which constituted the chamber wall. Today, there are at least fourteen different methods with variations for cooling the combustion devices and nozzles of liquid propellant, solid propellant, and/or nuclear rocket propulsion engines. It is the intent of this paper to examine these methods, to describe for each the useful range of operating conditions, as well as present and likely future applications, to define their limitations and associated problems. Emphasis is primarily placed on liquid rocket engines."
  • spc_horn_000087.pdf

    From the summary: "Both [guidance] schemes steer toward a specified end point. The MIT scheme uses thrust to cancel out the effective gravity, a nonlinear term, which may be inefficient in certain cases. The MSFC scheme is more closely connected with calculus of variations and optimization theory in a reasonable degree of approximation."
  • compflowcont.pdf.pdf

    Presented are the results of a study comparing four proposed control systems for the first stage flight of Saturn V launch vehicles. The primary basis of comparison is the effect on structural loads, using the bending moments at three stations as load indicators. Two of the systems sense only the vehicle attitude and attitude rate, while the other two systems also sense the lateral acceleration. A yaw plane wind response analysis, including rigid body translation, rigid body rotation, four bending modes, five slosh modes, and a non ideal control system, was performed. The winds used in the study were the Marshall synthetic profile and three selected Jimsphere-measured real wind profiles. Load relief obtained from the addition of accelerometer feedback in the control loop amounted to about 10 percent at maximum bending moment station. In view of predicted structural capabilities of the vehicle, this reduction in loads was not considered sufficient to offset the added complexity and the slight reduction in rigid body stability .
  • Decaofspacprog.pdf.pdf
  • descst124m.pdf.pdf

    This report is a description of the ST124-M inertial stabilized platform system and its application to the Saturn V launch vehicle. It is a summary report providing the system concept and not a theoretical presentation. Mathematical equations were included only where necessary to describe the equipment; however, the detail derivations supporting these equations were not presented since this was not the theme of the paper.
  • descst124minerstab.pdf.pdf

    This report is a description of the ST-124M inertial stabilized platform system and its application to the Saturn V launch vehicle. It is a summary report providing the system concept, and not a theoretical presentation. Mathematical equations were included only where necessary to describe the equipment; however, the detailed derivations supporting these equations were not presented since this was not the theme of the paper.
  • spc_stnv_000034.pdf

    Digesu worked in the Astrionics Division of MSFC. This paper was presented at the AIAA Guidance & Control Conference, Massachusetts Institute of Technology, Cambridge, Massachusetts, August 12-14, 1963.
  • Defense_Billboard_60_001.pdf
  • http://dkdayton.net/roberts/images/r04c/pdfs/r04c04-03.pdf
  • spc_stnv_000054.pdf

    Presented at the Fourth International Conference on Fluid Sealing held in conjunction with the 24th annual meeting in Philadelphia, May 5-9, 1969.
  • spc_stnv_000055.pdf

    This paper presents a discussion of a hybrid simulation used to dynamically verify the Saturn Guidance and Control subsystems. First, the Saturn vehicle is briefly described to provide background information. The Instrument Unit (IU) is considered in more detail to give a proper setting for the Guidance and Flight Control (G and FC) discussion that follows. After a brief description of the actual G and FC System operation, simulation models of the G and FC components are considered in detail. This is followed by a discussion of the model assignment to a particular computer (digital or analog) and justification for making that assignment. Finally, results of the AS-204/LM1 hybrid simulation studies are briefly considered with mention of the actual flight data.
  • spc_stnv_000064.pdf

    Written by NASA Office of Manned Space Flight Associate Administrator George E. Mueller, this is an article from G. E. Challenge, Fall 1966, page 26 to 32.
  • ssfmanewteltec_031307114348.pdf

    A technique new to telemetry is discussed which promises to alleviate an enigma facing the telemetry engineer : How to adequately transmit the avalanche of vibration and other wideband data desired in the development phase of large missiles and launch vehicles. The data channels are stacked in the frequency spectrum as single sideband subcarriers which frequency modulate the RF carrier. The system design utilizes to advantage the statistical properties of vibration data to achieve maximum data transmission efficiency from the available RF carrier deviation. However, in contrast to proposed statistical predigestion techniques, the data is transmitted in raw form.
  • uah_hockey_003.pdf

    This flier advertises a trip to Maine for UAH hockey fans to see "the Chargers capture the top-ranked Black Bears of the University of Maine." Tours of Maine scenery and sites, a "New England Style Dinner," lodging, and transportation are offered in the package.
  • spc_stnv_000109.pdf

    This paper includes the equations for the bending moment of a launch vehicle with the effects of bending and sloshing dynamics. It also includes a comparison between the bending moment response envelope of the measure winds and the bending moment response of the MSFC synthetic wind profile.
  • spc_stnv_000110.pdf

    This paper, presented at the fifth annual Reliability and Maintainability Conference in New York City, contains a "prime contractor's reliability program for components/parts for the Douglas S-IVB stage project." These parts include special flight critical items and their complementary reliability engineering program plan is outlined in this paper.
  • http://dkdayton.net/roberts/images/r10/pdfs/r10_02-06.pdf
  • Progplaneart_012709164341.pdf

    Manned space flight offers the opportunity to couple the astronaut/scientist's ability to select and process data and to calibrate, modify and repair instruments with the vantage point for astronomical observations provided by a platform located above the Earth's atmosphere. This paper briefly examines the role which manned space flight may play in the 1970-1990 time period in meeting astronomy research needs. The instruments and facilities which appear feasible for that period are described.; Paper presented by J. R. Olivier, National Aeronautics and Space Administration, George C. Marshall Space Flight Center and H. L. Wolbers, Ph.D, McDonnell Douglas Astronautics Company - Western Division, Advance Space and Launch Systems.
  • Defense_Billboard_31_001.pdf

    Woman's purse and shoe on street outside of a bar as a cab drives away
  • Realtimeopersyst_101507115951.pdf

    Presentation aimed to encourage a final check on the Saturn V project before its first launch to ensure safety and success.
  • spc_stnv_000112.pdf

    This paper was presented at the International Cryogenic Engineering Conference in Kyoto, Japan. It details the use of cryogenic technology in rocketry and how its usage created "many new techniques and deeply stimulated many fields of cryogenic technology."
  • spc_mcca_000160-63.pdf

    Prepared by Librarian Christel L. McCanless and presented to the Arts and Sciences Committee on Huntsville Degree Program. The document includes a review of library materials and an outline of future plans, including comparisons to collections at other universities.
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