Browse Items (86 total)

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  "Management Plan for Saturn Vehicle System."

  The purpose of this management plan is to set forth the channels 1 and methods used by the National Aeronautics and Space Administration for the development of the SATURN Vehicle System, This plan is based i on past experience and proven management principles of the Development Operations Division, The attached figures illustrate the plan.
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  "Michoud operations : historical operations: July 1, 1963 - December 31, 1963."

  Historical report from July 1st to December 31st.
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  "Management matrix integrating logistics support planning events."

  This was found folded inside Configuration Management. Taken from Defense Industry Bulletin, June 1968. Includes an organizational chart and an accompanying bibliography.
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  "Saturn IB orientation training manuel."

  Prepared through joint efforts of Personnel Department, Education and Development Branch, Systems Training Unit, Michoud Operations and Engineering Communications Department, Technical Information Branch, Applied Communications Engineering Section, Huntsville Operations.; This publication presents a brief descriptive summary of the Saturn IB vehicle and Chrysler's Corporation's accomplishments in the missiles and space field. The Saturn IB information presented herein is based on current plans for each of the stages. Although there may be design changes from vehicle to vehicle, the basic components, systems, and operating principles will remain similar to previous models.
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  "Purchasing and contracting at the George C. Marshall Space Flight Center."

  This is a speech given to fellow purchasing agent regarding purchasing and contracting.
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  "Fulfilling the Aerospace Engineer's Responsibility for Product Reliability."

  The management techniques described in the paper support the Saturn S-IVB Program which is being conducted for the National Aeronautics and Space Administration, Marshall Space Flight Center.
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  "Saturn S-II stage program plan."

  This documents outlines the S & ID plan to fulfill the requirements of Contracts NAS7-80 and NAS7-200 for the design, development and manufacture of the Saturn S-II stage.; APPROVED by R E. Greer, Vice President and S-II Program Manager.; This reissue supersedes all previous issues of this report.; FOREWORD: The S-II stage is 81.5 feet in length and 33 feet in diameter, with a usable propellant capacity of 970,000 pounds, The S-II propellants are fully cryogenic-liquid oxygen at -279 F and liquid hydrogen at -423 F. Its five-engine cluster provides one million pounds of thrust. The stage is a cylindrical structure of relatively light weight with a shell designed to resist all loads without the use of stiffening members. Its skin is of welded aluminum panels, as are the elliptical bulkheads of the fuel and oxidizer tanks. Unique to its design is the common bulkhead that separates the -423 F liquid hydrogen from the -247 F liquid oxygen. The common bulkhead - a sandwich of two 33-foot diameter aluminum domes separated by an insulating filler of honeycomb - eliminates the weight penalty that would be imposed by the second bulkhead in more conventional design. This document describes the S & ID program plan for development of the S-II stage and associated a support equipment.
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  "Response to any news media queries concerning MSFC S-II stage."

  Letter to answer any incoming questions from the media regarding the MSFC-II stage and any briefed on Seal Beach.
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  "Project Manager's Report."

  Report detailing the costs of materials and contracts.
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  "Saturn Vehicle Cryogenic Programs."

  Paper from the 1965 Cryogenic Engineering Conference at Rice University, Houston, Texas, paper K-4. The abstract states, "This paper covers the cryogenic propellant and gaseous application to the George C. Marshall Space Flight Center Saturn Programs. Emphasis is placed on the overall application and the resultant logistic considerations. The planning of facilities, storage, and transportation required to ensure an adequate supply of cryogenic fluids when needed is traced from the engine and stage requirements. The entire cycle of technical requirements, estimating the quantities required from production and management of the program is developed, spacecraft application and other trends that affect cryogenic production are reviewed."