Browse Items (8023 total)

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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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  "MSFC technical facilities history and description."

  This document includes a brief history of MSFC facilities, defunct names used by various Redstone located missile organizations, Michoud facilities history, the Slidell Operations Office history, the Mississippi Test Facility (MTF) history, and detailed description of technical facilities for the MSFC R&D Laboratories. The final section presents a detailed breakdown of property and facility values for various MSFC facilities over a period of time.
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  "MSFC project descriptions : 1967."

  A directory of different projects with descriptions underneath.
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  "Organization chart of the Department of Defense - Directory."

  An organizational chart directory.
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  "Press release 931A : Saturn S-IV first firing."

  Following is text of Douglas release on successful first firing of clustered P&W RL10 engines. Occurred at 11:12 A.M. PDT, August 17. Santa Monica, California.; "Sacramento, Calif,--Man's effort to reach the moon moved nearer reality today with the successful first firing here of the six liquid oxygen-liquid hydrogen fueled engines of the Saturn S-IV.
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  "Reliability engineering program provisions for Space System contractors. Revision 2."

  This document was cited in the Saturn contracts before NPC-250-1 was written. The sense of this document is the backbone of NASA reliability today and has become a generally accepted element of engineering rationale.
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  "Saturn I/IB quarterly film report no. 24, April, May and June, 1965."

  A list of film reports covering the months of April, May and June of the year 1965.
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  "Rocket engine turbo pumps for space travel."

  Finding the turbopump arrangement which is best suited for a given rocket engine - space travel applications - constitutes an important task. The arrangement depends upon a large variety of different factors, such as, the engine cycle, weight, the liquids to be pumped, the cavitation performance, the bearings and their lubrication, the seals and the turbine. In this report these factors and their influence on the turbopump configuration are discussed. It is shown that three of them: weight, propellants to be pumped and obtainable suction performance have the largest influence on the selection of the turbopump. A systematic approach is outlines for the design process, which allows to arrive at a turbopump arrangement best suited for a given application.
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  "Report From Mississippi."

  Report detailing the progress NASA's Mississippi test facility has made testing the Apollo-Saturn rocket.
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  "Saturn stages S-II : July 7, 1961 : Minutes of the phase II pre-proposal conference for stage S-II procurement."

  Transcription of a confrence aiming to propose ideas for new rocket designs. Includes references to slides.