UAH Archives, Special Collections, and Digital Initiatives

Browse Items (204 total)

  • spc_stnv_000149.pdf
  • Binder1_080108093849.pdf

    The Abstract states "The four checkout systems developed and utilized by the National Aeronautics and Space Administration (NASA) for acceptance checkout of the Saturn V launch vehicle stages and instrument unit are described. The vehicle's characteristics, test policies, equipment design criteria, and operational factors are reviewed. Following a general description of each checkout system, this paper presents a brief definitive description of each major subsystem test station. These test systems are used for post-manufacturing and post-static firing acceptance checkout. The section related to the S-II stage includes several representative flow diagrams and descriptions of automatic tests. To present in detail the large volume of information describing these four checkout systems would require the writing of four papers."
  • spc_stnv_000065.pdf
  • Binder1_080610113218.pdf

    The document is an annotated bibliography of reports from Requested by D. L. Christiensen. 2
  • spc_stnv_000130.pdf

    Includes change pages. Contract NAS8-14000. Second revised edition. V66-15610. NASA-CR71607. The introduction notes, "This second revised edition of the Astrionics System Handbook has been developed under the direction and overall supervision of Dr. Rudolf Decher of the Astrionics Systems Engineering Office. This description of the Saturn Astrionics System has been generated by personnel of the Astrionics Laboratory, the staff of the Astrionics Systems Engineering Office, and by personnel of the International Business Machines Corporation working under Contract NAS8- 14000. The handbook will be updated and expanded as it becomes necessary due to changes or refinements in the system concept and hardware. Sections not contained in the first release of this document will be made available within three months." Signed by Ludie G. Richard, Chief, Systems Engineering Office, Astrionics Laboratory. The document is missing pages in the following locations: Chapters 8, 9, 12. Sections 15.2, 15.3, 15.4-1 thru 15.4-16, 15.5-1 thru 15.5-2, 15.5-5 thru 15.5-8.
  • spc_stnv_000130.pdf

    This updated edition of the Astrionics System Handbook instructs, "The enclosed pages change, delete, or supplement the information in the Astrionics System Handbook (1 August 1965). Insert these pages and destroy the pages they replace."
  • spc_stnv_000069.pdf

    This copy is a reproduction of a document held by the NASA Scientific and Technical Information Facility .
  • Binder1_062508100607.pdf

    The document is a list of tools from the Manufacturing Engineering Laboratory at MSFC. Included in the list are the tool numbers, titles, and stages of development. Prior to the list the document includes a handwritten note from Bill Vardaman. Issue April 1968. Office R-ME-TDP.
  • Binder1_070908082349.pdf
  • 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."
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