USRA Houston Repository

Browsing by Subject "Lunar laser ranging"

Browsing by Subject "Lunar laser ranging"

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  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1970)
    Parts and materials used in the Array are listed on the attached sheets which reflect the three subassemblies of the array for the Apollo 14 Flight Unit: A. Panel Structure Assembly B. Insulation Assembly C. Retro-Reflector ...
  • Anthis, W. (Bendix Aerospace Systems Division, 1970)
    Parts and materials used in the Array are listed on sheets which reflect the three subassemblies of the array: A. Panel Structure Assembly B. Insulation Assembly C. Retro-Reflector Array Assembly.
  • Unknown author (The University of Texas. McDonald Observatory, 1974)
    In this report we will review both the operational as well as research activities which occurred during the last fiscal year, the fifth year of regular operation. We will close the report with an assessment of our current ...
  • Wainio, K. (Bendix Aerospace Systems Division, 1970)
    The results of the Pointing Analysis conducted for the Apollo 14 LRRR Experiment are presented. The analysis provides parameters for the design of the LRRR alignment mechanisms. The Littrow site was the basis for the analysis.
  • Wainio, K. (Bendix Aerospace Systems Division, 1970)
    The results of the LRRR pointing analysis conducted for the new Apollo 14 lunar landing site (Fra Mauro) are presented. The analysis provides parameters for the design of the LRRR alignment mechanism.
  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1970)
    The report has been arranged to reflect the qualification rationale differences between qualification and flight for Apollo 14, and LRRR qualification test results pertinent to evaluating its readiness for final acceptance.
  • Anthis, W. (Bendix Aerospace Systems Division, 1970)
    It is the intent of this preliminary report to reflect the qualification rationale and summarize the qualification test plan for the LRRR Qual model. This report will be finalized to support Flight Model delivery and will ...
  • Granholm, E. A. (Bendix Aerospace Systems Division, 1970)
    The results of thermal analyses performed on the Apollo 14 LRRR to determine operating temperature levels and heat exchange between the Array and Structure Assembly are contained herein.
  • Howell, F. L. (Bendix Aerospace Systems Division, 1971)
    Parts and materials used by A. D. Little, Inc. in the 300 corner LRRR Array Assemblies A & B are listed on the attached sheets.
  • Wainio, K. (Bendix Aerospace Systems Division, 1971)
    This report summarizes the results of the Apollo 15 LRRR (300 Corner) Pointing Analysis. This analysis provides the parameter values for the array tilt angle and shadow mark angle, each of which are necessary to properly ...
  • Howell, F. L. (Bendix Aerospace Systems Division, 1971)
    It is the intent of this final report to reflect the qualification rationale and summarize the qualification test plan results for the LRRR Qual model.
  • Kuechenmeister, T. J. (Bendix Aerospace Systems Division, 1971)
    The following compilation of Crew Engineering reports documents the human factors considerations that influenced the LRRR (300) design and the LRRR (300) deployment plans.
  • Micocci, Angelo J. (Bendix Aerospace Systems Division, 1970)
    The following compilation of Crew Systems and Operations human factors engineering design inputs to the LRRR Design Group constitutes the changes required to modify the Apollo 11 LRRR design to the Apollo 14 configuration.
  • Marrus, Leslie D. (Bendix Aerospace Systems Division, 1971)
    The following compilation constitutes the Crew Engineering LRRR(300) design inputs to the LRRR(300) Design Group.
  • Redick, Ronald L. (Bendix Aerospace Systems Division, 1971)
    This ATM discusses the results of Crew Engineering deployment of the LRRR concept model by a pressure suited subject, and recommendations for design improvements. resulting from the evaluation.
  • Marrus, Leslie D. (Bendix Aerospace Systems Division, 1970)
    The following compilation of Crew Systems and Operations reports documents the human factors and systems analysis considerations that influenced the LRRR design and the LRRR deployment plans.
  • Marrus, Leslie D. (Bendix Aerospace Systems Division, 1969)
    This EATM presents the EASEP deployment task/time sequence analyses for the Laser Ranging Retro-Reflector (LRRR) and the Passive Seismic Experiment Package (PSEP). Separate and combined task/time deployment sequences for ...
  • Marrus, Leslie D. (Bendix Aerospace Systems Division, 1970)
    This specification defines the performance, design, construction, and interface requirements for the Crew Training Model of the Laser Ranging Retro-Reflector (LRRR). This model is a mechanical simulation of the LRRR (300) ...
  • Redick, Ronald L. (Bendix Aerospace Systems Division, 1970)
    On March 25 the Crew Systems and Operations group performed a pressure suited, 1 G deployment of the LR3 Mock-Up. The purpose of the test was to evaluate the astronaut interface in the areas of manipulative characteristics, ...
  • Anthis, W. (Bendix Aerospace Systems Division, 1970)
    The purpose of the Failure Modes and Effects Analysis (FMEA) is to discover critical failure areas in a system and to remove susceptibility to such failures. Each possibility of failure is considered in light of its ...

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