UAH Archives, Special Collections, and Digital Initiatives

Browse Items (6320 total)

  • loc_salm_000134_000135.pdf
  • loc_salm_000132_000133.pdf
  • loc_salm_000130_000131.pdf

    The note on the reverse of the photo adds that Vernon was "200 lbs. of fighting spirit."
  • loc_salm_000128_000129.pdf
  • loc_salm_000126_000127.pdf
  • loc_salm_000124_000125.pdf

    A sign for "Cafe Dingbat" can be seen in the background.
  • http://dkdayton.net/roberts/images/r02g/pdfs/r02g07-15.pdf
  • Binder1_071910091943.pdf

    The document's mission summary states "This documet is perpared jointly by the Marshall Sapce Fligh Center Laboratories S&E-ASTR-S, S&E-AERO-P, and S&E-ASTN-ESD. The document presents a brief and concise description of the AS-506 Apollo Saturn Space Vehicle and the AS-506 mission. Where necessary, for clarification, additional related information has been included. It is not intended that this document completely define the Space Vehicle, its sytems or subsystems in detail. The information presented herein by text and sketches, describe launch preparation, ground support activities, and the space vehicle. This information permits the reader to follow the sequence of events beginning a few hours before liftoff to mission completion."
  • IMG_2808.jpg

    This is a photo of the Bust of Sir Hans Sloane in the British Library. This is a replica of Sir Sloane's bust in the British Museum by Rysbrack. This bust is in the library because of Sir Sloane's contributions to the library.
  • dynloaofalauvehduetoinfwin_121307141031.pdf

    Analysis of the stability and dynamic load environment of a launch vehicle resulting from atmospheric disturbances is a very complex problem. To determine the dynamic load environment of the vehicle requires an adequate description of the wind field, vehicle dynamics and control system. The essential of such a study, namely methods of analysis, wind field specification and representative vehicle response parameters for evaluation, are of equal importance. This paper is concerned with the mathematical foundations of the vehicle model and method of analysis.
  • 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.
  • theuseofwindsheainthedesiofaerovehi_103107103412.pdf

    Prepared for presentation at the 23rd Meeting of the Structures and Materials Panel, AGARD, October 4-11,1966, ONERA, Paris, France.; ABSTRACT: The relative influence of various wind profile properties and disturbances on launch vehicle flight dynamic response is studied. Particular emphasis is placed on the influence of wind shears and turbulence on dynamic response during the boost phase of the flight. Four hundred and seven individual detailed (Jimsphere) wind profiles are the primary wind inputs for this analysis. Time response of the vehicle to each profile is computed and a statistical evaluation of the results made. Results are obtained for the Saturn V space vehicle and conclusions drawn as to the relative influence of wind shears and turbulence vs the degree of refinement of the dynamic model of the space vehicle.
  • Memoroutandlett_013108093853.pdf

    This document also contains part of the Business Week article "North American tries to advance under fire", (June 3, 1967) pages 154 to 162. The complete article can be found at the UAH Library in microfilm format.; The document has handwritten notes and is a poor photocopy.
  • loc_burw_-80.pdf

    The medical officer notes: "I certify that the above mentioned officer was sick while on leave and unfit to travel till 12-9-45".
  • spc_stnv_000102.pdf

    This appendix includes various diagrams of orbital launch vehicles, graphs of propellant and tankweight, returnpayload, and lift-off requirements, velocity requirements for a manned lunar mission, multiple drawings for the Saturn C-3 vehicles, lunar mission payloads, information of vehicle size, and a summary of the Saturn C-3 lunar mission.
  • recovsib_070207115020.pdf

    The paper deals with the selection of a simple recovery system for the Saturn IB first stage. As an introduction to the discussion on recovery system objectives, a plot of the expected trajectory is presented. This is followed by a statement which lists the necessary steps which must be followed to develop a recovery program.
  • spc_schu_0001872.pdf
  • telmesinsreqforsII1andsII2_020408135342.pdf

    Photocopy of an inspection list requirements for S-II-1 and S-II-2.
  • 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.
  • proincrypumdesforspaapp_031808115456.pdf

    Report detailing the problems surrounding cryogenic pump design for space travel and missions.
  • 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.
  • S1VBsathigh_032608091902.pdf

    The development of carrier rockets For manned space missions has been one of the major activities in the aerospace field during the past decade. The early space efforts were made possible by the existence of large ballistics missiles. It soon became obvious that the delivery of weapons and the launch of large spacecraft could not be combined into one operational system in an efficient way; therefore, a family of spacecraft boosters had to be created.
  • Advertisement for quinine.jpg

    An advertisement for two different quinine treatments for malaria; quinine bisulphate and quinine sulphate. Marketed as of "exceptional purity".
  • spc_spac_000162_000165.pdf

    This advertisement includes equipment specifications and features for the electronic band organ.
  • Somecompappl_011608101417.pdf

    This paper discusses a number of interesting applications of digital computers in the checkout of individual Saturn stages and in the prelaunch checkout of the complete Saturn vehicle. It discusses the concepts of automation in Saturn checkout, the unique two-computer mode of operation at the launch site and the operations of the high speed data link connecting the two computers. Also discussed are the functions of the computer while propellants are loaded automatically on one of the stages; the functions of the display computer in the newest and largest Saturn display system, and operations and utilization of the Digital Events Evaluator, the main recording device utilized during stage checkout.
  • spc_mcca_000100_web.pdf
  • telesystforsatus-istagdeve_032107081755.pdf

    The telemetry system used on the Saturn S-I stage for the transmission of vehicle test data is described. Multiplex and modulationtechniques such as PAM/FM/FM, SS/FM and PGM are used in the system. The diverse data requirements for developing the eight-engineliquid-fueled stage necessitated the use of a combination of severalmodulation techniques to efficiently handle the data. A cursory comparisonis made of the merits of each technique. Physical and electricalrequirements and characteristics of the system are outlined.
  • http://dkdayton.net/roberts/images/r04a/pdfs/r04a03-06.pdf
  • http://dkdayton.net/roberts/images/r04a/pdfs/r04a03-11.pdf
  • Friday__November_10__2017_at_11_59_55_AM_default_288347a7.mp4

    Dr. John Rogers is from Kansas, and in Kansas, John loved to drive out into the prarie and find places where there had been homesteads. There, he would lay on the ground and look up at the stars at night. This all inspired him to get involved with the space station, and human factors engineering. John received his Bachelor's degree at Kansas State University, and then he received his Master's degree at The University of Arkansas. At this point, he took up a teaching job in Arkansas, and during that period of time, he recieved a National Science Foundation summer research fellowship at Florida State University. There, John did research on the effects of radiation on the human body. After leaving his teaching job, he went to the University of Mexico to pursue his Phd. While he was there, he was able to be a part of a summer program that pushed him towards his career. Since John did such a great job at the summer program, they kept him on as a consultant where he could work unlimited hours, and work any time he wanted to. The work that he did there included: examining human air and organizations, and considering what was the common factor/the emphasis in the atomic energy. After his job there, he started working at NASA in June of 1967. His job tasks there included: looking at the simulations and to look at the experimental design. He also had to try to make sure that they had solid statistics behind their results that were being detained.
  • spc_nick_000326_000326.pdf

    Written by John F. Roehm, this report covers a summary of reports of Colonel John C. Nickerson, Jr.'s efficiency from his former Battery Executive Officer and regimental basketball boach.
  • http://dkdayton.net/roberts/images/r01b/pdfs/r01b01-03.pdf
  • vbas_space_journal_055_116.pdf

    This issue includes a statement announcing Space Journal's termination of all connections with the U.S. military and with the Rocket City Astronomical Association. At the time, commander of the Army Ballistic Missile Agency (ABMA) at Redstone Arsenal Gen. John B. Medaris was concerned that the publishers and writers, all in the employ of ABMA, were using their government positions for personal gain through the magazine. Topics covered in the issue include the dangers and feasibility of space travel, designing buildings for life on the Moon, and the existence of life elsewhere in the universe.
  • spc_mitc_001_062B.pdf

    This issue discusses at length the competition in science, technology, and engineering between the United States and the Soviet Union, including comparisons of developments in missiles, satellites, and educational systems. This issue also includes plans for a village on the Moon. Includes the subscription card inserted in the center of the issue.
  • spc_hinr_001_060a.pdf
  • spc_schl_007_058a.pdf
  • SpaceJournal_1957-Summer_LowResolution.pdf

    This issue of Space Journal includes articles written by Fred L. Whipple, Hermann Oberth, and Ernst Stuhlinger, as well as a foreword by Wernher von Braun. The issue also includes drawings for an observatory to be built at the top of Monte Sano Mountain in Huntsville, Alabama. Produced by the Rocket City Astronomical Association (now known as the Von Braun Astronomical Society), Space Journal was published in Huntsville from 1957 to 1959. This digitized copy was generously provided by Jeff Bennett at the Von Braun Astronomical Society (VBAS).
  • spc_nick_000186_000187_000289_000290.pdf

    Written testimony of Maurice W. Roche, administrative assistant for the Office of the Secretary of Defense, as presented if he were "present in court". Signed by the defense counsel, the accused, and the trial counsel.
  • http://dkdayton.net/roberts/images/r04a/pdfs/r04a08-00-001.pdf
  • http://dkdayton.net/roberts/images/r04a/pdfs/r04a08-01.pdf
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