UAH Archives, Special Collections, and Digital Initiatives

Browse Items (204 total)

  • 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.
  • spc_stnv_000139.pdf

    The document is designated for internal use only.
  • spc_stnv_000030.pdf
  • spc_stnv_000095.pdf

    This memorandum details changes or changes to be considered in Apollo-Saturn nomenclature. It also contains the matter of the Apollo and AAP missions designs and changes Seamans wishes to see.
  • spc_stnv_000133.pdf

    The abstract notes, "The development of an automatic pressure transducer calibration system is discussed in this report. Evolution from past practices and systems into an automatic calibration system with computerized data handling is described."
  • 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_000107.pdf

    According to an abstract found on the page following the title page, this paper includes "one possible conceptual definition of an early Apollo Logistics Support Systems (ALSS) is presented and various payloads for the system are briefly discussed. " It also discusses the Lunar Mobile Laboratory (MOLAB) and other considerations for a lunar scientific mission.
  • spc_stnv_000106.pdf

    Presented at the AIAA/AAS Stepping Stones to Mars Meeting, this paper compares the "payload velocity spectrum for existing and future missions" with Saturn V capabilities.
  • 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."
  • 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.