USRA Houston Repository

Browsing by Subject "Aerospace telemetry."

Browsing by Subject "Aerospace telemetry."

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  • Fox, T. W. (Bendix Aerospace Systems Division, 1970)
    This report presents a Failure Mode, Effects and Criticality Analysis (FMECA) performed on the Data Transmitter and documented in the attached worksheets.
  • Fox, T. W. (Bendix Aerospace Systems Division, 1970)
    This report presents the Data Transmitter reliability prediction estimates derived through the studies of Data Transmitter Failure Mode, Effects and Criticality Analysis (FMECA) and Data Transmitter Parts Application ...
  • Lanning, H. E. (Bendix Aerospace Systems Division, 1969)
    This document re-evaluates the ALSEP/MSFN communication performance margins as a result of performance measurements made upon existing ALSEP hardware.
  • Reeves, J. T. (Bendix Aerospace Systems Division, 1970)
    The purpose of this ATM is to define the carrier stability and to provide samples of typical stability data applicable to ALSEP's 1 through 4. The data presented should permit those interested in such potential use to ...
  • Coleman, C. W. (Bendix Aerospace Systems Division, 1967)
    Describes a system used to check out programs written to decommutate and process telemetry (TM) data in real-time.
  • Wallace, R. B. (Bendix Aerospace Systems Division, 1975)
    The Apollo 14 ALSEP downlink signal stopped on 1 March 1975. Efforts to regain a signal, by uplinking commands to switch to the redundant processor or transmitter, failed.
  • Bedford, A. (Bendix Aerospace Systems Division, 1972)
    This ATM summarizes the scope and contents of the calibration curve data book and calibration magnetic tape which will be supplied to the MCC for ALSEP Array E downlink data conversion. Certain of the Array data channels ...
  • Jensen, C. W.; Thomas, D. J. (Bendix Aerospace Systems Division, 1972)
    This report documents an investigation of the MSFN/ALSEP S-Band Compatibility Test Results and provides a rationale and recommendation relative to the test validity and relative to Command Decoder Circuit Modifications ...
  • Dallaire, Rodney J.; Thomas, D. J. (Bendix Aerospace Systems Division, 1971)
    This ATM provides the reliability justification for the redundancy method employed in the Array E (Apollo 17) uplink. The Array E uplink employs standby redundancy without cross-over and automatic switch-over after 61 hours ...
  • Unknown author (Lyndon B. Johnson Space Center, 1976)
    Contains test procedures to be used for validating the compatibility of Spacecraft Tracking and Data Acquisition Network to Mission Control Center and their readiness to support the ALSEP program.
  • Swanson, R. C. (Bendix Aerospace Systems Division., 1971)
    This specification defines the performance, electrical interface and design requirements for the ALSEP Array E System Test Set Data Unit.
  • Patrick, A. E.; Logan, Joseph C. (Lockheed Electronics Company, Houston Aerospace Systems Division, 1969)
    To verify the command link from the unified S-band Manned Space Flight Network (MSFN) to the Apollo Lunar Surface Experiments Package (ALSEP), a series of tests was performed at the Manned Spacecraft Center at Houston, ...
  • Reeves, J. T. (Bendix Aerospace Systems Division, 1969)
    High temperature functional tests were performed on Prototype Transmitter SN-5 and Qualification Transmitter SN-8 to determine operating characteristics of ALSEP data transmitters in the high temperature possible at EASEP ...
  • Douthat, D. Z. (Bendix Systems Division, 1966)
    Five of the sixteen channels of the analog multiplexer in the Active Seismic data processor have been as signed for central station measurements. These five will be the only telemetry on the central station during Active ...
  • Pistor, H. (Bendix Systems Division, 1966)
    Contains all items of telemetry and commands in Array A.
  • Lanning, H. E. (Bendix Aerospace Systems Division, 1969)
    This analysis determines the maximum allowable antenna pointing error for the telemetry and command links based upon a 0 db performance margin for either nominal or worst case conditions for communication margins to be maintained.
  • Douthat, D. Z. (Bendix Systems Division, 1966)
    This memo recommends that 4 or 5 central station events be packed into a single analog channel and shows a simple method for doing this.
  • Taylor, J. (Bendix Aerospace Systems Division, 1969)
    The purpose of this ATM is to document the Parts Application Analysis (PAA) for the S-Band transmitter designed and manufactured by the Bendix Aerospace Systems Division for use in ALSEP Flight System 2A. The data contained ...
  • Fox, T. W. (Bendix Aerospace Systems Division, 1970)
    This ATM documents the Parts Application Analysis (PAA) performed on the Data Transmitter and its Telemetry circuitry.
  • Smith, S. (Bendix Aerospace Systems Division., 1972)
    This specification establishes the requirements for performance, design, test and qualification of a high reliability PSK transmitter which will provide at least a 1. watt S-band output while operating for 2 years in a ...

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