UAH Archives, Special Collections, and Digital Initiatives

Browse Items (970 total)

  • SatuVgrouwindprog_091207152652.pdf

    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.
  • dynpro.pdf.pdf

    Addresses improving spacecraft safety by resolving various known dynamic problems.
  • satvapoflicon_060508122521.pdf

    Diagram displaying the internal rooms, pieces and functions of the Saturn V as well as the space-suits of the astronauts.
  • furnbrazliqurock_061407145410.pdf

    Brazing as a technique for joining metal parts has been utilized for centuries. Industry, however, has only begun to use it on a wide scale in the last twenty years. The rapid growth of brazing has been a result of consumer and military demands Tor products of lighter weight, less expense, and higher performance. Today, brazing is one of the most widely used fabrication techniques in the production of liquid rockets, gas turbines, refrigerator and other types of heat exchangers, automobile parts, vacuum tubes, and many nuclear products.
  • Meetwithdire_111808165933.pdf

    The following people participated in an all day meeting at ABMA Huntsville on 6 January 1960: Dr. W. Von Braun, Mr. E. Rees, Mr. A. Hyatt, Mr. A. Siepert. Writer of the memorandum is Abraham Hyatt, Deputy Director, Launch Vehicle Programs.
  • Manaplancomp_120108133922.pdf
  • Crewbrieinst_012309113213.pdf

    Document outlining different slides of a presentation containing numerous organizational charts, diagrams and bullet-list points.
  • instunitnavsatib_082407113528.pdf

    Within the first 10 minutes of NASA's initial Saturn IB flight, the Instrument Unit (IU), nervecenter of America's mightiest launch vehicle, is designed to make more than 7 million calculations, sample vehicle calculations 100 times a minute, telemeter 3 million numbers back to Earth, and measure the performance of 300 pieces of equipment in the IU, S-IB, and S-IVB stages.
  • Crewbrieinst_012709172107.pdf

    Document outlining different slides of a presentation containing numerous organizational charts, diagrams and bullet-list points.
  • Instunitprogrevi.pdf

    Handwritten names and phone numbers on the first page. Apollo / Saturn Team.