UAH Archives, Special Collections, and Digital Initiatives

Browse Items (8023 total)

  • Michassyfacteldir_072908145639.pdf
  • michoudops_062607124250.pdf
  • Milestonesincryoliqproproceng_041508144818.pdf

    This paper reviews the milestones achieved with cryogenic liquid propellant rocket engines, discusses current technology improvement programs, and projects future engine designs. During the last two decades, these cryogenic rocket engines have played a major role in rocketry and achieved numerous important milestones. These engines power the Vanguard, Redstone, Thor, Atlas, and Titan I vehicles , the Saturn I and Uprated Saturn I vehicles, and will soon be employed in the Saturn V for the Apollo missions. The requirements dictated by these vehicles have necessitated growth from the 27,000-pound-thrust Vanguard engine to the 7,600,000-pound-thrust booster cluster for the Saturn V. Gains in specific impulse have also been significant. The successful application of liquid hydrogen in the Centaur and Saturn upper-stage rocket engines was a major achievement.
  • loc_burw_-103.pdf

    The record contains Edwin D. Burwell Jr.'s personal information, military history, and insurance notice.
  • minimax_081607145436.pdf

    Keith D. Graham is principal mathematician, Systems and Research Center, Honeywell, Inc., 2345 Walnut Street, St. Paul, Minnesota.; Work done under NASA contract NAS 8-11206 from the George C. Marshall Space Flight Center.; ABSTRACT: A method of specifying the gains of a linear controller for a large launch booster using a new application of optimal control theory is described in this paper. Results for a specific example are included. An important control requirement is to maintain cost variables (such as bending moment, engine gimbal deflection, and lateral deviation from desired trajectory) within specified limits in the presence of load disturbances. This requirement is met by using a performance index which depends explicitly on maximum achievable values of the cost variables in a finite time interval.
  • misandfacofinsdevbra_060508143335.pdf

    Describes the purpose and goes of the George C. Marshall Space Flight Center. Instrumental development branch.
  • misstesttorr_030209160511.pdf

    Description of a photograph of a rocket static test firing.
  • monte_sano_1938_web.pdf

    The map notes park roads, buildings, telephone lines, trails, overlooks, and cliffs, and includes drawings of picnic and camping areas, a pool, and a lodge. Locations such as Inspiration Point, the former site of the Monte Sano Hotel, Natural Well, O'Shaughnessy Point, the fire tower, and the C.C.C. camp are marked. The map was taken from "aerial photographs as drawn by O.G. Graves" based on a land survey conducted by John F. Davis.
  • spc_mcca_001_002.pdf

    "A spectacular view from Monte Sano State Park near Huntsville, Alabama. Color by Wayne Floyd."
  • http://dkdayton.net/roberts/images/r04a/pdfs/r04a13-33.pdf