Browse Items (2178 total)

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  "Chronology of early Air Force man-in-space activity: 1955 - 1960."

  The foreword states "In this chronology, Air Force manned space flight activity is viewed from the perspective of the ballistic missile development agency - the Air Research and Development Command's Western Development Division, later re-named the Air Force Ballistic Missile Division. Due to resource limitations at the Space Systems Division historical office, research for this chronology has been generally limited to materials available in the files of that office. All documents cite in the notes which follow each entry are located in the archives of the Historical Division, Office of Information, Space Systems Division, in Los Angeles California." There are handwritten notes throughout.
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  "This is Your Chrysler Saturn Story."

  The document is a booklet created as part of the NASA/Chrysler Corporation Space Division manned flight awareness program. It discusses Chrysler's role in manufacturing and testing the Saturn and includes photographs and diagrams of Saturn stages, operations at Michoud, testing, and future missions. The section headings included in this booklet are "Chrysler and the Saturn," "Saturn at Michoud," "The Voyage of Saturn," "Saturn Firings," and "Saturn's Missions."
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  "Cleaning and Contamination Control."

  The document is a paper describing contamination cleaning methods and advocating for further developments in the field. Tables and figures are included at the end of the paper. The figures include a comparison of Saturn V with Saturn I and Saturn IB and cross-sections of the Saturn C-5, S-IC stage fuel tank assembly and oxidizer tank assembly.
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  Guided Missiles Range Division Clipper, vol. 2, no. 3, October 1961.

  The Clipper is a Guided Missiles Range Division, Pan American World Airlines, Inc., internal publication. This issue includes the articles "News at a Glance," "The Big One," "New Ships on the Horizon," "Civic Responsibility," "Picture Highlights," "Service Awards," "September Service Pins," and "Recognizing Credit Union." "The Big One" includes details about Pan Am's role in developing the Saturn booster.
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  Combustion oscillations in the F-1 engine, monthly report.

  The set of documents includes an introductory letter written by D. Brainerd Holmes and Tischler's report with the subject "F-1 Combustion Instability Report for Associate Administrator; Period June-July 1963."
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  Combustion Oscillations in F-1 Engine.

  The set of documents includes an introductory letter written by D. Brainerd Holmes and Tischler's report with the subject "F-1 Combustion Instability Report for Associate Administrator; Period March-April, 1963".
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  "The Common Bulkhead for the Saturn S-II Vehicle: Unique Manufacturing Effort Adds to Space-Age Hardware Technology".

  Presentation regarding the construction of Apollo and Saturn rockets.
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  Comments on SA-5 mission.

  A notation in the upper lefthand corner states "For the record: These are Dr. von Braun's comments to present to President Kennedy during his visit at Cape Canaveral, Fla., Nov. 16, 1963." A handwritten note is in the upper right corner. It appears that some of the pages to this document are missing.
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  "Comments on Problems Relating to the Lunar-Landing Vehicle."

  "This technical note concerns some of the problems encountered with the landing of a payload on the moon. The main problem areas such as guidance, velocity control and impact considerations are discussed. Although no final conclusions or designs are intended, it is hoped that the material presented will serve as a guide for future detailed work."
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  "A Comparison of Advanced Cooling Techniques for Rocket Thrust Chambers".

  The document is a technical paper for Astronautics and Aerospace Engineering Magazine.The copy has handwritten notes that appear to be for revisions. The abstract states "In the early days of rocket propulsion, two primary methods were employed for cooling the walls of thrust chambers. These were uncooled metal chambers where the heat sink capacity of the chamber and nozzle wall materials limited the operating duration, and regeneratively cooled chambers where one of the propellants was circulated in a cooling jacket which constituted the chamber wall. Today, there are at least fourteen different methods with variations for cooling the combustion devices and nozzles of liquid propellant, solid propellant, and/or nuclear rocket propulsion engines. It is the intent of this paper to examine these methods, to describe for each the useful range of operating conditions, as well as present and likely future applications, to define their limitations and associated problems. Emphasis is primarily placed on liquid rocket engines."