UAH Archives, Special Collections, and Digital Initiatives

Browse Items (8239 total)

  • LettMSFCAttnDrWernVonBraun_090408155515.pdf

    Letter to Wernher von Braun from NASA headquarters regarding Project Highwater and how it was withheld.
  • loc_gold_000346_000346.pdf

    Company secretary, Harry A. Newman, writes to the stockholders informing them of a special meeting where stockholders will be asked to authorize changes in per value to the capital stock.
  • loc_hutc_000206_000217.pdf

    Most likely William Wyeth Newman, these various checks are signed by W. W. Newman from the W. R. Rison Banking Company to various recipients.
  • loc_hutc_000218_000221.pdf

    Written on Phoenix Assurance Co., Ltd. letterhead, these pages contain handwritten notes and calculations by W. W. Newman that begin in the 1890s and runs through 1903.
  • loc_hutc_000225_000226.pdf

    Will writes to Ellen about his trip to Canada. He includes various activities and details of the weather.
  • PRATTW~1.PDF

    Photograph of a Pratt & Whitney rocket engine.
  • loc_gold_000397_000398.pdf

    Newson writes to Milliken about a party who wants to purchase Dallas Mfg. Co. stock though the dividends are low. The second letter details the purchase price the party is willing to pay and if Milliken knows anyone with 100 to 300 shares for sale.
  • satsivcryoweighsyst-I_072007112534.pdf

    In order to achieve maximum vehicle efficiency, it is essential that the vehicle propellants be loaded to desired values and that these propellants approach simultaneous depletion at the end of powered flight. To accomplish precise loading and assure minimum residuals, a highly accurate and repeatable, vehicle located, propellant management (PM) or propellant utilization (PU) system must be used. As the ability to load propellants to predetermined values depends directly on the ability of the system to accurately sense the propellant masses, it is essential that the system be calibrated with respect to propellant mass under conditions resembling those to be experienced during final loading and powered flight. The use of a cryogenic weight system will reduce the unknown factors in capacitance sensor element shaping, tank geometry, and propellant properties to a degree which will permit the determination of propellant masses to with .025%.
  • spc_nick_000112_000112.pdf

    Nichols writes to Bell to inform him of the supoena he received to appear in court on July 2nd. He states that he will proceed as requested unless he hears from Bell with other instructions.
  • spc_nick_000565_000565.pdf

    Nichols writes regarding a letter he received from Lt. Col. Barry that may be of some interest to Bell and the Nickerson case.