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  • Kuechenmeister, T. J. (Bendix Aerospace Systems Division, 1971)
    Since the lifetime goal of the LRRR(300) is 10 years it is desired to minimize degrading or disabling conditions which could be brought about by LM. Potential damage to the LRRR could be caused by excessive heat, dust or ...
  • Lavin, W. J. (Bendix Aerospace Systems Division, 1971)
    The purpose of this ATM is to perform a "worst case" analysis of LSG/Boyd Bolt interface using the data recorded at the tests performed at Arthur D. Little Incorporated on 15 July through 21 July 1971 to determine the ...
  • Gerke, P. Donald (Bendix Aerospace Systems Division, 1972)
    Describes the science characteristics of the Lunar Surface Gravimeter (LSG) Flight Model.
  • Bendix Corporation. Aerospace Systems Division. (Bendix Aerospace Systems Division., 1971)
    The Lunar Surface Gravimeter electronics technical description.
  • Wallace, R. B. (Bendix, Aerospace Systems Division, 1975)
    The sensor beam of Flight Lunar Surface Gravimeter (LSG) has been centered by partially uncaging the lunar masses. In this configuration the sensor exhibits a 1. 5 Hertz oscilation. Attempts to duplicate this configuration ...
  • Dela Cruz, M. (Bendix Aerospace Systems Division, 1971)
    A computer analysis of the closed loop performance of the flight sensor was performed on 15 September.
  • Van Hoorde, G. R. (Bendix Aerospace Systems Division, 1971)
    The purpose of this ATM is to document the results of the Parts Application Analysis study performed on the LSG Experiment. The stress levels shown were determined on the basis of electronic piece parts operating at the ...
  • Van Hoorde, G. R. (Bendix Aerospace Systems Division, 1971)
    The purpose of this ATM is to comment on the results of the single point failure analysis conducted on the lunar surface gravimeter experiment. It is to be noted that this ATM does not include single point failure analysis ...
  • Glowacki, R. E. (Bendix Aerospace Systems Division, 1967)
    This unscheduled ATM describes the test results obtained in pre-integration testing of the LSM Engineering Model.
  • Lavin, W. J. (Bendix Aerospace Systems Division, 1971)
    This Detailed System Hazard Analysis Report consists of two major sections; (1) The Detailed Fault Hazard Analysis and (2) The Fault Tree Logic Diagrams which evaluate the hazard potential of the LSP explosives during the ...
  • Min, G. B. (Bendix Aerospace Systems Division, 1971)
    The purpose of this ATM is to estimate from theoretical considerations the probability of fragments from an LSP explosive package striking the ALSEP Central Station.
  • Jones, Joseph P. (Bendix Aerospace Systems Division, 1972)
    Identifies all conditions under which the explosive components of the LSP are manufactured, tested, transported, and stored while under the cognizance of the Bendix Corporation, Aerospace Systems Division (BxA). Sufficient ...
  • Jones, Joseph P. (Bendix Aerospace Systems Division, 1972)
    The Operation Hazard Analysis evaluates all known hazards identified throughout the operational life cycle of the LSP Experiments. This analysis supplements the Detailed Hazard Analysis (ATM 1049 ).
  • Jones, Joseph P. (Bendix Aerospace Systems Division, 1971)
    Early in the preliminary design phase of the Lunar Seismic Profiling Experiment (LSP), it was recognized that the environmental conditions to which the timer watch movements would be exposed on the lunar surface would cause ...
  • Toelle, Dan. (Bendix Aerospace Systems Division, 1971)
    This ATM revision presents a supplement to the study of the LSPE High Explosive Package and transport frame stowage thermal constraints subsequent to LM touchdown and prior to lunar deployment. In addition, lunar deployment ...
  • Toelle, Dan. (Bendix Aerospace Systems Division, 1971)
    This ATM presents the study of LSPE High Explosive Package and transport frame stowage thermal constraints subsequent to LM touchdown and prior to lunar deployment.
  • Toelle, Dan. (Bendix Aerospace Systems Division, 1971)
    This ATM provides an answer to Action Iten: 521, "BxA agreed that if explosive packages are exposed to the sun for 5 hours prior to each EVA, the 40° F timer requirement will be met. BxA to revise applicable ATM with ...
  • Toelle, Dan. (Bendix Aerospace Systems Division, 1972)
    This ATM Summarizes the analytical and test results of the Lunar Seismic Profiling Experiment Thermal Control Systems. The first section introduces the hardware and develops the mathematical thermal model of the explosive ...
  • Unknown author (Bendix Aerospace Systems Division, 1972)
    The purpose of this ATM is to (1) review the Lunar Seismic Profiling Experiment Safe-Arm Slide failure which occurred at the United States Naval Ordnance Laboratory (NOL). (2) evaluate the cause of the failure, (3) review ...
  • Weir, P. (Bendix Aerospace Systems Division, 1972)
    The purpose of this ATM is to document the results of a Thermal Battery test for the Lunar Seismic Profiling Experiment (LSPE).

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