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Browsing by Subject "Passive Seismic Experiment (Instrument)"

Browsing by Subject "Passive Seismic Experiment (Instrument)"

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  • Howell, F. L. (Bendix Aerospace Systems Division, 1971)
    The purpose of this ATM is to provide a qualification-by-similarity rational to SN03, the PSE model of the previous ALSEP System QSL.
  • Wilson, H. W. (Bendix Aerospace Systems Division, 1969)
    This memorandum presents the current inventory of commands applicable to the Passive Seismic Experiment Package. This revision reflects changes in the initial functional mode of the equipment as it is delivered to the lunar ...
  • Courtois, D. A. (Bendix Aerospace Systems Division, 1969)
    The purpose of this EATM is to present the results of a study of the power balance of the PSEP. The nominal operating conditions and the power balance effects of commands are described. The effects of the inadvertent ...
  • Courtois, D. A. (Bendix Aerospace Systems Division, 1969)
    The purpose of this EATM is to update the description of the functional aspects of the PSEP Power Subsystem, incorporating the effects of recent changes. The functional description is presented in a series of plots of ...
  • Wilson, H. W. (Bendix Aerospace Systems Division, 1969)
  • Howell, H. R. (Bendix Aerospace Systems Division, 1969)
    The purpose of this EATM is to describe the transient performance of the EASEP/PSEP system during the first lunar day, sunset, and sunrise on the second day. The results of this study have been used to determine the best ...
  • Johnson, P. A., 1938-; Kornemann, W. (Bendix Aerospace Systems Division, 1970)
    This ATM summarizes test data derived from the PSEP Qualification, Flight Acceptance, and the Qualification Retest and compares these data with analytical predictions. The Qualification Retest was conducted so that an ...
  • Courtois, D. A. (Bendix Aerospace Systems Division, 1968)
  • Wilson, H. W. (Bendix Aerospace Systems Division, 1969)
    This memorandum provides revised planning information on the special activities necessary to prepare PSEP for flight, to initiate lunar operation and to establish the proper conditions for lunar night survival and subsequent ...
  • Jones, Joseph P. (Bendix Aerospace Systems Division, 1970)
    This report covers a modified PSE Sensor Heater circuit increasing total power dissipation from 2.5 watts to 5.5 watts principally by replacing existing components with components of higher power ratings. Particular attention ...
  • Hiebert, Robert W. (Bendix Aerospace Systems Division, 1971)
    This addendum updates the System Failure Mode, Effects and Criticality Analysis (FMECA) for the Passive Seismic Experiment (PSE) Array A-2D, and E to the date of this addendum.
  • Deppe, R. H. (Bendix Aerospace Systems Division, 1971)
    On January 22, 1971, the BxA Crew Engineering group performed a lG, space- suited handling and deployment test with the PSE decoupled shroud mockup. The purpose of the test was to determine if a space-suited deployment of ...
  • Unknown author (Teledyne Earth Sciences., 1968)
    This technical manual provides operation and maintenance instructions for the Passive Seismic Experiment Subsystem, Part Number: 233000, manufactured by Teledyne Industries, Earth Sciences Division, Pasadena, California ...
  • Schmidt, R. A. (Bendix Aerospace Systems Division, 1967)
    This ATM provides data on the Passive Seismic Experiment Thermal Shroud stowing and handling procedure based on the prototype model procedure received from Teledyne/Earth Sciences Division.

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