USRA Houston Repository

Browsing ALSEP Documents by Title

Browsing ALSEP Documents by Title

Sort by:Order:Results:

  • Array E S-Band compatibility test results analysis 
    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 ...
  • Array E Subpack I dynamic analysis 
    Min, G. B.; Wadleigh, K. H. (Bendix Aerospace Systems Division, 1971)
    This ATM presents the results of the dynamic analyses performed on two different versions of ALSEP Array E - Subpack I. One version contained the Lunar Surface Gravimeter ( LSG) experiment, among others, while the other ...
  • Array E system description 
    Bedford, A.; Kasser, Joe E.; Thomas, D. J. (Bendix Corporation, Aerospace Systems Division, 1972)
    This ATM describes the ALSEP Array E System. Its main purpose is to convey an understanding of the Power and Data Subsystems operation to a depth just above the circuit schematic level.
  • Array E system grounding philosophy 
    Wallace, R. B. (Bendix Aerospace Systems Division, 1971)
    This ATM briefly describes modifications to system grounding philosophy from those applied on previous flights and provides system, component, and experiment grounding details.
  • Array E time/cycle sensitive list 
    Hendrickson, J. E. (Bendix Aerospace Systems Division, 1972)
    The time/cycle sensitive list for Array E is shown below. These parts are the only ones in which a possibility exists that they may be operated or cycled close to their design limit.
  • Array E uplink redundancy method justification 
    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 ...
  • ASE data format 
    Zimmer, J. (Bendix Systems Division, 1966)
    This ATM is written in response to Action Item B6-0805-5B requesting Bendix to evaluate the Stanford proposed data format.
  • ASE geophones and mortar box assembly alignment tests 
    Micocci, Angelo J. (Bendix Aerospace Systems Division, 1967)
    This ATM contains the reports on two (2) tests performed to determine astronaut capability to align the ASE Mortar Box Assembly (MBA)/geophones to the required limits of azimuth accuracy without a sophisticated sighting mechanism.
  • ASE grenade transmitter frequency drift 
    McDowell, J. R. (Bendix Aerospace Systems Division, 1971)
    This ATM provides a projection of the maximum frequency of the Flight 5 and Spare Active Seismic Experiment (ASE) grenade transmitters up to 6 years from transmitter acceptance testing.
  • ASE off-equatorial thermal study 
    Wright, N. (Bendix Aerospace Systems Division, 1970)
    The purpose of this ATM is to summarize the results of an in-house thermal study conducted to evaluate the thermal performance of the Active Seismic Experiment (ASE) for the current landing site latitude specification range ...
  • ASE qualification test 
    McDowell, J. R. (Bendix Aerospace Systems Division, 1969)
    This ATM has been prepared (per Qual C QTRR RFC 1-2) to correlate the overall qualification testing of the Active Seismic Experiment (ASE) and the Final Reports will collectively document the qualification results.
  • ASE redesign evaluation 
    Griffin, J. (Bendix Aerospace Systems Division, 1971)
    This ATM summarizes the Bendix evaluation of the ASE pallet design and subsequent results of the test program conducted at Langley Research Center to verify the adequacy of the ASE design and deployment modifications during ...
  • ASE Review Team report 
    Harris, J. D. (Manned Spacecraft Center., 1971)
    The ASE Review Team has reviewed the data from the ASE vacuum firing test, established the test validity, reviewed the ASE development history, and performed specific studies described in this report.
  • ASE Review Team report : EH4 -R13 
    Wiseman, Donald G. (Lunar Surface Project Office, Manned Spacecraft Center, 1971)
    The ASE Review Team has reviewed the data from the ASE vacuum firing test, established the test validity, reviewed the ASE development history, and performed specific studies described in this report.
  • ASE/CE 16 ch. multiplexer -A/D converter reliability prediction and failure mode, effects & criticality analysis 
    Dallaire, Rodney J. (Bendix Aerospace Systems Division, 1970)
    This ATM documents the Reliability Prediction and Failure Modes Effects & Criticality Analysis of the Bendix designed ASE/CE 16 CH Multiplexer A/D Converter. The analysis reflects the final flight configuration for the ...
  • ASE/CE 16 ch. multiplexer -A/D converter reliability prediction and failure mode, effects & criticality analysis 
    Dallaire, Rodney J. (Bendix Aerospace Systems Division, 1970)
    This ATM documents the Reliability Prediction and Failure Modes Effects & Criticality Analysis of the Bendix designed ASE/CE 16 CH Multiplexer A/D Converter. The analysis reflects the final flight configuration for the ...
  • Assessment of two year ALSEP Array E capability 
    Hendrickson, J. E. (Bendix Aerospace Systems Division, 1972)
    Considers specific subjects related to ALSEP two year life expectancy, namely: Reliability Predictions; Time/Cycle Sensitive Items; Previous ALSEP Lunar Operations; Thermal/Power Prediction vs Time; and Qualification Levels.
  • August and September system safety progress report ALSEP Array E. 
    Bendix Corporation. Aerospace Systems Division. (Bendix Aerospace Systems Division, 1971)
    This ATM documents the progress of the System Safety Program for ALSEP Array E (Apollo 17) through September 1971.
  • Band mechanism for cask retention 
    Dewhirst, D. L. (Bendix Systems Division, 1967)
    This ATM outlines the structural considerations pertinent to the band mechanism which supports the graphite cask.
  • Bendix Corporation (Crawler-Transporter / ALSEP) 
    Unknown author (Bendix Aerospace Systems Division, 1969)
    Two documents together Apollo Lunar Surface Experiments Package on the Moon .... Tranquillity plus two years and Apollo Lunar Surface Experiments Package (ALSEP) Both from Bendix Aerospace Systems Division

Search HOU Repository


Browse

My Account