Browse Items (970 total)

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  "Saturn V Apollo flight configuration."

  Diagram displaying the internal rooms, pieces and functions of the Saturn V as well as the space-suits of the astronauts.
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  "Saturn V Apollo lunar orbit rendezvous mission."

  Diagram explaining the process of a lunar mission from liftoff to recovery.
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  "Saturn V derivatives."

  This paper desciibes an evolutionary family concept of !h turn V derivative launch vehicle systems, discusses their performance capabilities, and outlines their ability to perform orbital and hlgh-energy missions at minimum total program cost.
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  "Saturn V first stage annual progress report : fiscal year 1966."

  This report is the consolidation of D5-11994, "Quarterly Technical Progress Report," for the fourth fiscal quarter and the fiscal year 1966 Annual Progress Report and places special emphasis on activities on the fourth fiscal quarter.
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  "Saturn V First Stage Annual Progress Report: Fiscal Year 1968."

  The report covers June 30, 1967 through June 27, 1968: Contract NAS8-5608, Schedules 1 and 1A, July 27, 1968. Prepared by J. P. Delaloye, Management Reporting and Analysis; Supervised by D. G. Valentine, Management Reporting and Analysis; Approved by R. F. Terry, Program Reports; D. H. Creim, Michoud, Program Planning and Reporting Manager; E. K. Cooper, S-IC Program Executive.
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  "Saturn V ground winds program."

  The concept on Saturn V was to "budget" an amount for the dynamic portion of the wind load as a factor on the steady state drag. Wind tunnel tests paralleled the development and fabrication phases. The results indicated that the system was unable to withstand the design winds; thus, a decision was made to implement a viscous damper "fix" on the facility vehicle at the Kennedy Space Center. Damping tests in the Vertical Assembly Building (VAB) will have been completed and response tests on the pad will be in progress at the time of this symposium. This paper will present the history and status of this program to date.
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  "Saturn V inboard profile : Launch escape system flight separation."

  Diagram displaying the launch escape system flight separation in progress.
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  "Saturn V interface management."

  The purpose of the Saturn V Interface Management System is to establish and maintain interface design compatibility between interfacing items under the design responsibility of different agencies. It provides the management tools for effective change control over the design of designated systems and equipment that have critical interface design requirements.
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  "Saturn V launch vehicle ground support equipment fact booklet."

  This booklet has been prepared to provide a quick reference to Saturn V stage peculiar ground support equipment. It consists of visual presentations and a brief description of each major component. It is intended to quickly familiarize concerned elements with the over-all MSFC launch vehicle ground support equipment and is not intended for design usage. The booklet has been prepared in five sections. Section I contains the introductory material and a description of the Saturn V mobile launcher (ML). Section II contains information on the umbilical equipment. Section III contains information on the servicing equipment, both fixed and mobile. Section IV contains information on the access equipment. Section V contains information on the handling and auxiliary equipment.
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  "Saturn V quarterly progress report : January - March."

  Quarterly progress report for the months of January - March, 1966.