Browse Items (970 total)

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  "The program manager's problem"

  Included in "First Annual Logistics Management Symposium," Huntsville, Alabama; Archive copy is a poor photocopy. Describes the stages of rocket-development/launch and the logistical problems with each.
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  "Telegraphic message : inspection requirements for S-II-1 and S-II-2 at KSC."

  Photocopy of an inspection list requirements for S-II-1 and S-II-2.
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  "Recoverable S-IB."

  The paper deals with the selection of a simple recovery system for the Saturn IB first stage. As an introduction to the discussion on recovery system objectives, a plot of the expected trajectory is presented. This is followed by a statement which lists the necessary steps which must be followed to develop a recovery program.
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  "Appendix to Chapter II of a Survey of Various Vehicle Systems for the Manned Lunar Landing Mission."

  This appendix includes various diagrams of orbital launch vehicles, graphs of propellant and tankweight, returnpayload, and lift-off requirements, velocity requirements for a manned lunar mission, multiple drawings for the Saturn C-3 vehicles, lunar mission payloads, information of vehicle size, and a summary of the Saturn C-3 lunar mission.
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  "Memorandum, routing slip, and letter by Harold G. Russell, Colonel, USAF, concerning the Business Week article 'North American tries to advance under fire.'"

  This document also contains part of the Business Week article "North American tries to advance under fire", (June 3, 1967) pages 154 to 162. The complete article can be found at the UAH Library in microfilm format.; The document has handwritten notes and is a poor photocopy.
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  "The use of wind shears in the design of aerospace vehicles."

  Prepared for presentation at the 23rd Meeting of the Structures and Materials Panel, AGARD, October 4-11,1966, ONERA, Paris, France.; ABSTRACT: The relative influence of various wind profile properties and disturbances on launch vehicle flight dynamic response is studied. Particular emphasis is placed on the influence of wind shears and turbulence on dynamic response during the boost phase of the flight. Four hundred and seven individual detailed (Jimsphere) wind profiles are the primary wind inputs for this analysis. Time response of the vehicle to each profile is computed and a statistical evaluation of the results made. Results are obtained for the Saturn V space vehicle and conclusions drawn as to the relative influence of wind shears and turbulence vs the degree of refinement of the dynamic model of the space vehicle.
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  "A Practical Approach to the Optimization of the Saturn V Space Vehicle Control System Under Aerodynamic Loads."

  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.
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  "Dynamic Loads of a Launch Vehicle Due to Inflight Winds."

  Analysis of the stability and dynamic load environment of a launch vehicle resulting from atmospheric disturbances is a very complex problem. To determine the dynamic load environment of the vehicle requires an adequate description of the wind field, vehicle dynamics and control system. The essential of such a study, namely methods of analysis, wind field specification and representative vehicle response parameters for evaluation, are of equal importance. This paper is concerned with the mathematical foundations of the vehicle model and method of analysis.
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  Technical information Summary Apollo-11 (AS-506) Apollo Saturn V Space Vehicle.

  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."
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  "Technical History of Saturn."

  Draft of working paper. Typed with handwritten notes (title and author) and pages. Copy in MSFC files noted on first page.