UAH Archives, Special Collections, and Digital Initiatives

Browse Items (970 total)

  • Testlaboprogfeb1966_083007095938.pdf

    Monthly rogress report for the test laboratory regarding the Saturn 1B program between Feburary and March
  • Testlaboprogrepomay121966tojune121966_110107111326.pdf

    Monthly rogress report for the test laboratory regarding the Saturn 1B program between Feburary and March
  • TEstlabprogrep2_031008111252.pdf

    Laboratory monthly progress report for the Saturn 1B program between dates August 1st through August 31st, 1967.
  • TEstlabprogrep3_032408084650.pdf

    Laboratory monthly progress report for the Saturn 1B program between dates July 1st through July 31st, 1967.
  • TestlabprogrepDEC_051408095158.pdf

    Laboratory monthly progress report for the Saturn 1B program between dates December 1st through December 31st, 1967.
  • TestlabprogrepOCT_041808091527.pdf

    Laboratory monthly progress report for the Saturn 1B program between dates October 1st through October 31st, 1967. Page 17 missing.
  • Testoperorgachar_120408111035.pdf

    Organization Chart of the North American Rockwell Test Operations.
  • Testprocvalidbycompsimulation_071508150442.pdf

    Digital computer simulation of the Saturn I Instrument Unit electrical networks was accomplished using the Discrete Network Simulation programs. The schematics were analyzed and a logic model prepared which consisted of a series of Boolean equations. The test procedures, which are written in the Acceptance, Test, or Launch Language (ATOLL), consist of a sequential set of computer instructions for the RCA llOA checkout computer to control the operation of the electrical networks. The procedures also contain the predicted results for each operation. The driving functions for the simulation of the model are generated from the ATOLL test tape by the Input Generator Program. The time sequenced operation of the networks is indicatedby the output from the simulation program in addition to the number of times each component in the system changes state. The results of the simulation are compared to the test procedure predictions on the ATOLL tape by the Comparator Program and any differences are listed. The Comparator Program also lists any component which did not change state at least once.
  • Thedeveofacheclangatol_110907113826.pdf

    ATOLL was developed to fulfill the requirements for a common computer language that could be used by the test engineers for launch and factory checkout. "ATOLL" is the abbreviated name for Acceptance, Test, Or Launch Language.
  • thedevofaboncombulforsat_090707133327.pdf

    A Part of the development of the Saturn S-IV/S-IVB stage the Douglas Aircraft Company has pioneered in the development of the cryogenic common bulkhead. The term common bulkhead is derived from the design function of the bulkhead, which is to separate the two cryogenics, liquid hydrogen and liquid oxygen, in a single tank, thereby shortening the stage and eliminating the necessity for two separate bulkheads and the associated interstage structure. The common bulkhead is structurally adequate to withstand both the thermal and the pressure loads from both the hydrogen and the oxygen tanks, and it has sufficient insulation properties to prevent the liquid hydrogen from freezing the liquid oxygen. Another benefit from the common bulkhead is that it permits a reduction in the total length of the vehicle, thereby reducing the bending moments.