UAH Archives, Special Collections, and Digital Initiatives

Browse Items (970 total)

  • spc_stnv_000139.pdf

    The document is designated for internal use only.
  • 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.
  • spc_stnv_000094.pdf

    This memorandum contains the pages to be changed in the logistics program for the Apollo/Saturn Project. The logistics plan includes the design, procuring, manufacturing, and production processes. This plan formalizes the program, improves logistic support, and implements management and action plans.
  • Faciengi_121508155406.pdf

    Article makes references to a film. Centers around the idea that testing space vehicles extensively before launch is cost control.
  • manpofacmakfut_021208085025.pdf

    This paper presents in synoptic form, an analysis of the management problems being faced in making fuhlre manned spaceflight decisions. It is an attempt to view the manned space program in total perspective - its relationship to other scientific research, other national programs, the role of Congress, the President's role, industry's role, and then show their relative influence and impact on decisior, making for the Post-Apollo period.
  • builmoonrock_082007101725.pdf

    "Building the Moon Rocket" was presented at the National Machine Tool Builders Association Meeting, Doral Beach Hotel, Miami, Florida on November 3, 1965 by Dr. Mathias P.L. Siebel, the Deputy Director, Manufacturing Engineering Laboratory. There are handwritten notes throughout.
  • Vonbraumoveende_072910160005.pdf
  • scanstich_072210162848.jpg

    News article that details the creation and function of a lunar module or "moon bug" created by Wernher von Braun.
  • spc_stnv_000115.pdf

    This memorandum contains artificial gravity considerations for Project Apollo and was directed to Seamans, Wernher von Braun, Donlon, and Gilruth. Silverstein writes that he believes it is too early to tell if the Apollo spacecraft is capable of providing artificial gravity.
  • TechsurvABMA_111808164326.pdf

    Handwritten notes on the document.; Archive copy is a poor photocopy.
  • Roleofvonbraulett_121108095421.pdf

    Memorandum from NASA Chief of Public Affairs to Eugine M. Emme. States that a video from Wernher von Braun are included regarding his views on the NASA program.
  • iupresdedi_080207152456.pdf

    This is a note book that contains newspaper articles and photographs about the new IBM building in Huntsville, Alabama. It also has information about the Instrument Unit for the first Saturn IB flight. There is also information about the Saturn IB Instrument Unit being barged to Kennedy Space Center.; There are 2 pages that list the articles with the title, newspaper name, writer and date.; There are six color photographs that show the dedication of the IBM building and the Instrument Unit. One photograph has Dr. Wernher von Braun standing behind the ring. Two of the photographs show the Instrument Unit on a trailer being pulled by a truck.; Preferred Citation: [Identification of item] Saturn V Collection, Dept. of Archives/Special Collections, M. Louis Salmon Library, University of Alabama in Huntsville, Huntsville, AL.
  • Spacstatoper.pdf.pdf
  • histrockdevsm.pdf

    A document recounting the history of the Rocketdyne Development Division
  • Binder1_071910110656.pdf

    The Preface states "This is a directory of industry, University, and Federal contacts who are involved in the areas of Management Science, Behavioral Science, Operations Research , Cybernetics, and Organizational Structure and Behavior. The listing represents a variety of disciplines -- Sociology, Psychology, Social Psychology, Psychiatry, Anthropology, Statistics, History, Public Administration, Political Science, Economics, Systems Analysis, Ecology,and General Systems Theory."
  • TechProbOnBo_062408092345.pdf

    For the purposes of this paper, an onboard checkout system is defined as a system which is built into prime flight equipment, flies with it, and permits a checkout capability to exist during all the major phases of the test and mission life of that prime equipment. Varying degrees of capability may exist in such a system, depending on what is designed into it. This, in turn, is generally dependant on life and mission requirements of the prime equipment, degree of mission checkout required, reliability restrictions,redundancy levels, data management scheme, and equally important, state of the art . Not all checkout can be accomplished with onboard equipment. Mechanical system problems such as leak detection, for example, require techniques that cannot be remotely controlled and evaluated today. On the other hand, such things as in-flight telemetry have been used for quite a long time and will continue to be used for onboard checkout.
  • Casecomp_091907132002.pdf

    "The Case for Compatibility" is a paper by Robert L. Smith, Jr., who worked in Quality and Reliability Assurance Laboratory at George C. Marshall Space Flight Center. The summary states, "Ever since the use of missiles and space launch vehicles began, questions have existed in every program regarding the similarity between upstream (e.g., manufacturing, static firing ) and launch site checkout equipment. Programs have existed which utilized nearly identical equipment for both uses; other programs have existed in which any resemblance of the equipment was probably coincidental. Many factors have entered the final decisions, not the least of which were economic and schedule considerations, and, in some instances, the organizational structure of the developer."
  • pracautomanufcheck_051107090838.pdf

    This paper presents a number of solutions to a number of unanswered questions regarding the Saturn projects.
  • facidesihandliqhyd_051107104601.pdf

    Presented to German Society for Rocket Technology & Astronautics.Essay discussing the capabilities of liquid hydrogen as fuel.
  • Fabrsatus-icboos_081407122702.pdf

    AIAA Second Annual Meeting, San Francisco, California. Discusses the fabrication process of the Saturn S-IC booster.
  • Letttodrwern31464_120908091357.pdf

    Archive copy is a poor photocopy. Unable to read.
  • Intewithdrwerh52564_121008163244.pdf

    Transcription of an interview with Wernher von Braun and Mr. Sohier.
  • memoinditomsfccircandmsfcadmireguandprocchiemanaservoffims-ch_112607141847.pdf
  • Binder1_081110135224.pdf

    The document is a Space Task Group report to the president. Pages 8, 18, 26, 27 of the document are missing.
  • SaturnIBSA217_052008142122.pdf

    This document contains a definition of a reference Saturn IB launch vehicle designated SA-217. The Saturn IB SA-217 is a projected reference vehicle, based on Saturn IB SA-212, incorporating the latest proposed product improvements. The two-stage payload capability of this vehicle to a 100-nautical-mile circular orbit is 44,965 pounds. The Saturn IB SA-217 launch vehicle is to be used as the baseline vehicle for advanced studies requiring the use of the standard or modified Saturn IB launch vehicle. This vehicle definition does not necessarily represent approved changes to any specific vehicle. This document supersedes the Saturn IB SA-213 reference Launch Vehicle, described in memorandum R-P&VE-DIR-65-92.
  • spc_stnv_000065.pdf
  • satIfliteseval_070507143020.pdf

    As this paper is being written, the Saturn I flight test program includes five flights launched between October, 1961 and January, 1964. All five fiights were complete successes, both in achieving all major test missions and in obtaining an unprecedented volume of system performance data for flight analysis.
  • sdsp_skyl_000070_001.pdf
  • enggcappresentation.pdf.pdf

    This Engineering Capabilities Presentation lists the competence and capability that has been demonstrated by the Space Support Division of Sperry Rand Corporation while fulfilling contractual commitments in the aerospace industry. This is a preliminary presentation; the preparation of a complete capabilities history of the division is currently in the developmental stage. The Capabilities Experience Summary is comprised of ten categories. e.g. Category 1 - Aeronautics, etc. The capabilities reported herein were performed by the Space Support Division under Contract NAS8-20055 to the National Aeronautics and Space Administration, George C. Marshall Flight Center, Astrionics Laboratory, Huntsville, Alabama.
  • earorbworkcapbrochA_021110095433.pdf.pdf

    A brochure designed to depict a competence and capability in the area of large earth-orbital workshops.
  • Sperrandmontprog_092910151001.pdf

    The following pages contain reports for each of the individual contract appendices covering technical progress and accomplishments, related problems, and staffing progress. The report of manhours expended against each appendix by schedule order is being submitted as a part of the financial management report.
  • TVsystapoltele_111307142704.pdf

    Focuses on the construction and future use of the Apollo space telescope. The components described in this paper except for those listed otherwise were designed by the Space Support Division of Sperry Rand Corporation to specifications established by NASA's Marshall Space Flight Center in Huntsville, Alabama. Appreciation is extended to MSFC for permission to publish this paper and for data and help provided for its preparation.
  • statsmodforsaturn_012508122337.pdf

    This report presents the logic leading to a mathematical expression for mission availability. Mission availability is treated as the probability that the cumulative downtime occurring during a mission of given length will be less than the time constraint. This is opposed to more general approaches such as steady state or instantaneous availability or operating time versus real time. We intend to present a practical and usable mathematical model by deduction and demonstration. The development is based on exponentially distributed downtimes. Experience shows that certain systems follow exponential downtime distributions except near zero. This error is often so small that it may be neglected. A future report will present a downtime distribution which will account for this small error.
  • P16608~1.PDF

    A letter to Jame E. Webb proposing that the first LEM that lands on the moon to be named after President Kennedy."
  • relipictmsfcphilstaffmgmt_031907142349.pdf
  • Reliqualmana_080707155107.pdf

    The role of Reliability and Quality in NASA program management is well defined by the NPC 200 series and complimentary procurement regulations.
  • reliasseliqurockengi_062107153119.pdf

    Proposed for the 10th National Symposium on Reliability & Quality Control. This paper will deal with various techniques of treatment of such data and associated graphic displays.
  • Lettmrgeorgemlow_120208120312.pdf

    Letter to George M. Lowe and Joseph F. Shea from H.A. Storms president continuing a conversation that was left unfinished.
  • Binder4_051208094654.pdf

    The abstract states "A telemetry system is a device to transfer information from an inaccessible to an accessible location. A constant input to a telemetry system yields outputs that are distributed according to some density function. A linear change in this constant input may yield a nonlinear change in output. The theory of statistics and experimental design may be applied to the data received from a flight to evaluate the inflight accuracy, linearity, and precision of various telemetry systems. This paper explains the analytical concepts used in postflight analysis of Instrument Unit telemetry systems. It also presents the method for interpreting the results of these analytical techniques."
  • Binder1_070908082349.pdf
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