USRA Houston Repository

Browsing by Subject "Laser Ranging Retroreflector Experiment"

Browsing by Subject "Laser Ranging Retroreflector Experiment"

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  • Failure modes and effects analysis 300 Array - LRRR 
    Howell, F. L. (Bendix Aerospace Systems Division, 1971)
    This memo contains the results of the final FMEA for the 300 Array LRRR experiment. This analysis has been revised and is now reissued as the final revision.
  • Human factors analysis effort for LRRR 
    Marrus, Leslie D. (Bendix Aerospace Systems Division, 1970)
    The following compilation of Crew Systems and Operations human factors analysis design criteria and requirements inputs to the LRRR Design Group constitutes the baseline parameters required to modify the Apollo 11 LRRR ...
  • Human factors analysis effort for LRRR(300) 
    Marrus, Leslie D. (Bendix Aerospace Systems Division, 1971)
    The following compilation of Crew Engineering human factors analysis design criteria and requirements inputs to the LRRR(300) Design Group constitutes the baseline parameters for the design of the LRRR(300),
  • Interface control specification for astronaut/LRRR (300) 
    Marrus, Leslie D. (Bendix Aerospace Systems Division, 1970)
    This specification establishes the requirements for the interface between the Laser Ranging Retro-Reflector (LRRR) experiment and the astronaut, while on the lunar surface.
  • Laser Ranging Retro-Reflector (LRRR) familiarization manual 
    Unknown author (Bendix Corporation, Aerospace Systems Division, 1971)
    Covers the scientific objectives of the lunar laser ranging experiment, the LRRR equipment makeup, deployment and operation. Covers the Apollo 11 and 14 experiments and the not yet deployed Apollo 15 reflector.
  • LRRR (300) task sequence/timeline for Hadley Rille Landing Site 
    Marrus, Leslie D. (Bendix Aerospace Systems Division, 1971)
    The attached LRRR (300) Task Sequence/Timeline for the Hadley Rille Landing Site provides a basic description of the astronaut operations required to completely deploy the Apollo 15 configuration of the LRRR (300).
  • LRRR (300) task sequence/timeline for Hadley Rille Landing Site 
    Marrus, Leslie D. (Bendix Aerospace Systems Division, 1971)
    The attached LRRR (300) Task Sequence/Timeline for the Hadley Rille Landing Site provides a basic description of the astronaut operations required to completely deploy the Apollo 15 configuration of the LRRR (300).
  • LRRR 300 Corner Array dynamic analysis 
    Goran, M.; Min, G. B.; Wadleigh, K. H. (Bendix Aerospace Systems Division, 1971)
    This ATM presents the results of the structural dynamics analysis performed on the Lunar Ranging Retro Reflector 300 Corner Array.
  • LRRR 300 thermal design final report 
    Granholm, E. A. (Bendix Aerospace Systems Division, 1970)
    The results of thermal design/analyses performed on the 300 corner Laser Ranging Retro-Reflector (LRRR 300) to determine array operating temperature levels, net array/lunar environment heat exchange, and corner optical ...
  • LRRR astronaut trainer acceptance test results 
    Redick, Ronald L. (Bendix Aerospace Systems Division, 1970)
    This ATM reports the results of the Crew Systems and Operations Acceptance Test for the LRRR Astronaut Trainer.
  • LRRR emplacement range and azimuth from LM 
    Cornille, H. (Bendix Aerospace Systems Division, 1970)
    Potential damage to the LRRR could be caused by excessive heat, dust or kapton contamination of the retro-reflector faces, or physical movement of the LRRR which produces misalignment.
  • LRRR emplacement range and azimuth from LM for Fra Mauro Landing Site 
    Cornille, H. (Bendix Aerospace Systems Division, 1970)
    Since the lifetime goal of the LRRR is 10 years it is desired to minimize degrading or disabling conditions which could be brought about by LM or other lunar equipment (ALSEP). Potential damage to the LRRR could be caused ...
  • LRRR pointing error analysis 
    Cornille, H. (Bendix Aerospace Systems Division, 1968)
    It is desired to have the LRRR reflector array oriented as nearly normal to the incident laser radiation as possible in.order to achieve a maximum returned signal. Various factors prevent the exact alignment, however, and ...
  • LRRR task sequence/timeline for Fra Mauro Landing Site 
    Marrus, Leslie D. (Bendix Systems Division, 1970)
    The attached LRRR Task Sequence/Timeline for the Fra Mauro Landing Site provides a basic description of the astronaut operations required to completely deploy the Apollo 14 configuration of the LRRR.
  • LRRR task sequence/timeline for Littrow Landing Site 
    Marrus, Leslie D. (Bendix Aerospace Systems Division, 1970)
    The attached LRRR Task Sequence/Timeline for the Littrow Landing Site provides a basic description of the astronaut operations required to completely deploy the Apollo 14 configuration of the LRRR.
  • LRRR(300) acceptance test deployment sequence 
    Geiss, H. W. (Bendix Aerospace Systems Division, 1971)
    The following deployment procedure is the Crew Engineering Acceptance Test Sequence for the LRRR(300) Trainer. This deployment sequence includes all the tasks and equipment manipulations that the astronauts will be required ...
  • LRRR(300) astronaut trainer acceptance plan 
    Geiss, H. W. (Bendix Aerospace Systems Division, 1971)
    The following is the Crew Engineering Acceptance Plan for the LRRR(300) Astronaut Trainer.
  • LRRR(300) astronaut trainer acceptance test results 
    Redick, Ronald L. (Bendix Aerospace Systems Division, 1971)
    The Acceptance Test performed by CS&O provides a means of evaluating the astronaut interface manipulative characteristics for the LRRR(300) Astronaut Trainer prior to delivery. CS&O personnel ensure that the LRRR(300) is ...
  • LRRR(300) emplacement range and azimuth from LM 
    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 ...
  • Structural analysis report Laser Ranging Retro-Reflector (300 corner) Apollo 15 
    Corcoran, J. F. (Bendix Aerospace Systems Division, 1971)
    This report consists of the stress analysis performed to substantiate the structural integrity of the LRRR-300 and all of its associated hardware.

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