UAH Archives, Special Collections, and Digital Initiatives

Browse Items (6320 total)

  • sdsp_skyl_000067_001.pdf

    This is a report about the Skylab 1 reentry.
  • Skywriterjun1369_121410150031.pdf

    News article covering NASA's announcement of Apollo 11's launch-date: July 16th.
  • Skywriterjun669_121410150523.pdf

    News article confirming NASA's announcement of Apollo 11's launch-day. Focuses on the optimism surrounding the launch as well.
  • spc_spac_000359_000360.pdf

    This flier has a colored image of the "Junior Hot Rod Ride" as well as a description and price for it.
  • JunoVspacvehi.pdf

    The initial phase of the JUNO V space vehicle development program, as presented herein, provides for a static demonstration and a total of four flight feasibility tests. The latter two flights will give the U.S. its first payload capability in excess of 10,000 lb in mid 1961. The objective of the overall program is to provide a reliable, economical, and flexible carrier vehicle with relatively large payload capability for orbital and space missions at the earliest possible date.
  • junovvehiclers_022107152001.pdf

    This report io the second in a scrics of reports on the JUNO V Space I Vehicle Development Program and indicates the present status of the overall I program. The objective of the overall program is to provide a reliable, economical, and flexible carrier vehicle with relatively large payload capability for orbital and space missions at the earliest possible date.
  • JunoVtransfeasstud_022807133058.pdf.pdf

    The purpose of this report is to present an investigation to determine the feasible, practical and economical method of transporting the JUNO V thrust unit. This includes the first phase of transporting between Fabrication Laboratory, Systems Analysis and Reliability Laboratory and to the test stand, as well as the later phases, onto the Redstone Arsenal loading docks and from there down the Tennessee, Ohio and Mississippi Rivers to the Atlantic Missile Range, Florida.; Transportation and Packaging Section, Systems Support Equipment Laboratory.
  • spc_dann_000222.mp4

    Clip shows the Dannenbergs (Konrad, Klaus, Betty, Ingeborg, and Kerry) celebrating Christmas. The family is shown lounging around a living room talking as Klaus plays with Kerry. Winter 1967.
  • spc_dann_000223.mp4

    Klaus, Kerry, Betty, and Ingeborg Dannenberg are shown opening presents around a Christmas tree. Winter 1967.
  • spc_dann_000224.mp4

    Footage of Klaus, Kerry, Ingeborg, and Betty Dannenberg relaxing around the Christmas tree. The video focuses mostly on Kerry and the Dannenbergs' new dog, a black terrier named McDuff. Winter 1967.
  • Keyeveninthe_120408112540.pdf
  • Keymsfcpersfor.pdf

    Essay detailing potential candidates for potential interviews.
  • spc_spac_000295.pdf

    The advertisement gives a description of the ride, its shipping weight, and its price.
  • spc_dann_000318.mp4

    Klaus and Jud Lynn hunt for Easter eggs and attend church service at St. Mark's Evangelical Lutheran Church. Spritime scenes around Huntsville.
  • spc_dann_000200.mp4

    Konrad, Klaus, and Ingeborg Dannenberg and the in-laws celebrate Christmas by opening presents in the family room at the Dannenbergs' house in Monte Sano, Huntsville, Alabama. Konrad Dannenberg's note on the film box reads, "ends w/ IMK Tired in chair." Winter 1963.
  • spc_dann_000317.mp4

    Klaus plays with other children and trims a rose bush with Ingeborg. Arrival of "Lilo and family", play with a small child in the front yard. Klaus takes a trip the playground and Monte Sano to hike and shoot his BB gun.
  • spc_dann_000198.mp4

    Klaus Dannenberg returns from sea and meets Konrad and Ingeborg in Atlanta, Georgia. While there, they stay at a Howard Johnson Inn and tour around Atlanta. 1963.
  • spc_dann_000197.mp4

    Klaus Dannenberg departs to join the U.S. Navy. Shown are Ingeborg and Konrad seeing him off before he boards a flight. Summer 1963.
  • spc_dann_000154.mp4

    First half of film shows Klaus Dannenberg being confirmed as well as the confirmation celebration at the Dannenbergs' house. Second half shows the new litter of kittens from the Dannenbergs' cat. Winter, 1957/58.
  • spc_dann_000205.mp4

    Shows the first part of Klaus Dannenberg's graduation from Auburn University. Film shows the in-laws going into the stadium and sitting down, as well as the graduates proceeding into the stadium. 1967.
  • spc_dann_000206.mp4

    Film from Klaus Dannenberg's graduation from Auburn University. Shown are a few clips from the president of the college, Klaus walking up to receive his degree, and Klaus meeting with family and friends afterwards. 1967.
  • spc_spac_000289_000292.pdf

    This advertisement provides images, features, and specifications for the turnstile.
  • kscaposatVmastespla_110207091724.pdf

    The John F. Kennedy Space Center (KSC) Apollo/Saturn V Development/Operations Plan, K-PM-0, establislies the requirement for an Apollo/Saturn V Master Test Plan (MBP). This document, prepared by the Saturn Systems Office.
  • scan0001_040709152818.jpg

    illustration of the L-UT/Armb umbilical tower
  • scan0001_040709152818.jpg

    illustration of the L-UT/Armb umbilical tower
  • LaunComp34Faci_062508095836.pdf

    Article detailing the different aspects of the Launch Complex 34 facilities.
  • LaunComp37Faci_062508141423.pdf

    Article detailing the different aspects of the Launch Complex 34 facilities.
  • Launcomp39faci_120307161856.pdf

    Article detailing the different aspects of the Launch Complex 34 facilities.
  • launcont_030209160221.pdf

    Description of an 8 x 10 inch black and white photograph.
  • launinfosatus-iv_062007154516.pdf

    The RL10, which powers the National Aeronautics and Space Administration' s Saturn S-IV, is the newest propulsion system to be put to work in advancing our nation's space effortr On November 27, 1963, a pair of RLlO's successfully powered a five-ton Centaur space vehicle in earth orbit in the first flight demonstration of the outer space powerplant which uses high-nenergy liquid hydrogen as fuel. A six-engine cluster of RLlO' s, generating a total of 90, 000 pounds of thrust, powers the Saturn S-IV stage. The 15, 000 pound-thrust engine was designed and developed for NASA's Mar shall Space Flight Center at Pratt & Whitney Aircraft's Florida Research and Development Center, 20 miles northwest of West Palm Beach.
  • sdsp_skyl_000017-000018.pdf
  • launvehiengiprojdeveplanjanu1,1967.pdf

    This revised edition of the Launch Vehicle Engines Project Development Plan supersedes the issue dated July 1, 1965. Significant changes which have been made are:- Removal of classified data to permit publication as an unclassified document; - Removal of material applicable to the RL-10 Engine Project which was transferred to the Lewis Research Center effective May 1, 1966; - Elimination of detailed schedules which quickly become obsolete; - Punched for maintenance in loose-leaf 3-ring binders and for ease in updating material through issuance of replacement sheets. Binders are not furnished. The information in this document is current to January 1, 1967.; The Launch Vehicle Engines Project Development Plan is established in accordance with requirements of NASA General Management Instruction 4-1-1, Planning and Implementation of NASA Projects, and OMSF Instruction MP 9320.044, Preparation and Revision of Program/Project Development Plans (PDP's). The Plan, herein referred to as the PDP, has been developed within the scope of current Apollo Projects Approval Documents (PADS) and will be maintained by the Engine Program Manager to identify program requirements, responsibilities, tasks, and resources, and time phasing of major actions required to accomplish the Engine Program.
  • lauvehengprodevpla_073007101313.pdf

    The primary mission objective of the 5-2 Engine Project is to continue development of a liquid oxygen/liquid hydrogen engine. capable of high-altitude restart. Both Saturn IB and Saturn V vehicles will use the J-2 engine; the S-IVB stage of Saturn IB vehicles and S-IVB stage of Saturn V vehicles will be equipped with a single J-2 engine. The S-I1 stage of Saturn V vehicles will use a cluster of five J-2 engines. Figure 1-3 illustrates these stages.
  • launvehirecosystrequ_061407154402.pdf

    The primary considerations in the design and development of a recovery system applicable to present expendable first stage launch vehicles are discussed. The general requirements that define the essential characteristics of a feasible recovery system are derived from three critical phases during flight. The degree of criticalness is primarily influenced by the conditions at stage cutoff and separation. The three critical phses of flight are broken down into the following: (1) conditions and requirements between stage separation to re-entry; (2) re-entry; and (3) terminal descent and landing.
  • Defense_Billboard_106_001.pdf
  • Defense_Billboard_43_001.pdf
  • Lettfrmwmet_011508085357.pdf

    Letter stating that "A review of the research origins of the Lance weapon system - Project Hindsight -Task 1 supplement" is inside as requested.
  • loc_burw_-63.pdf

    The orders grant Edwin D. Burwell Jr. seven days of leave to Great Britain.
  • Letttodrgeoremuel_120208110241.pdf

    This letter regarding designations for Apollo missions notes that "Unfortunately, the scheme for designating missions as stated in your message does not yet solve the problem of reserving the Apollo 1 name for Spacecraft 012 and its crew. As we have discussed with you and General Phillips in the past, the wives of the three deceased astronauts have made a special plea to reserve this Apollo 1 designation for Spacecraft 012 and the Grissom, White and Chaffee crew."; Archive copy is a photocopy.; In replay refer to: AB.
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