UAH Archives, Special Collections, and Digital Initiatives

Browse Items (970 total)

  • Satus-ic1965.pdf.pdf

    This Annual Progress Report has been prepared by the Boeing Company to fulfill the requirement under Article XXX, Paragraph A and C, Modification 100 of Contract, NAS8-5608 as amended by NASA letter I-MICH-DB, dated May 19, 1965, B. H. Aldridge to E. S. Olason. Subject: Change of NAS8-5608 to incorporate Quarterly Technical Progress into the Annual Progress Report.
  • d5-13197.pdf.pdf

    This Manufacturing plan is prepared in response to the Apollo Applications Program request for proposal No. 1.1.; PURPOSE: The purpose of this document is to present a Boeing plan for the manufacturing effort required to provide hardware and support for the installation and checkout of Experiment Packages and related equipment in the Apollo Systems Modules.
  • satuVfirsstagannuprogrepofiscyear1966_091207124644.pdf

    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.
  • Satuvlaun1967.pdf.pdf

    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.
  • Finatechreposatu.pdf
  • contprogproc_101007154101.pdf

    A collection of various procedures. Archive copy is a photocopy. There is no continuous numbering in this document.
  • Contprogprocedure_090308135708.pdf

    Outlines various procedures for Saturn V contractors.
  • boeing_060608144216.pdf

    The document is a Boeing manual. It contains operating procedures and directives specifically for the Launch Sytems Branch.
  • spc_stnv_000118.pdf

    This document includes the current basis for approval of ECPs, fatigue life after stress reduction, and other probability and comparative risk assessments. On the first page there is an inscription, "By E.L. Bombara NASA-MSFC."
  • devloxrp1eng_071807113246.pdf

    The development of liquid rocket engines follow similar patterns regardless of engine size. During the development of the H-1 and F-1 engines, many problems were encountered. Methods of solving the combustion instability problem are discussed. A description is given of the major components of each engine, outlining their unique features. The requirements for an insulation cocoon are discussed. Problems associated with materials substitution are provided; also highlighted is the fact that problems occur after engine deliveries and require continued development support. Safety features incorporated on the engines are mentioned. Solution to problems encountered in flight are discussed. Upratings of both engines systems are presented graphically.; On the NASA Technical Reports Server (NTRS) unclassified. Can also be found on AIAA.