USRA Houston Repository

Browsing by Author "Moskowitz, Lee S."

Browsing by Author "Moskowitz, Lee S."

Sort by:Order:Results:

  • 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 ...
  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1971)
    The purpose of this ATM is to document the results of the Parts Application Analysis study performed on the Power Conditioning Unit (PCU).
  • Moskowitz, Lee S.; Dallaire, Rodney J. (Bendix Aerospace Systems Division, 1970)
    This Failure Mode Effects and Criticality Analysis (FMECA) identifies those potential failure modes constituting single point failures or critical failures peculiar to ALSEP Flight System A2.
  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1971)
    This document provides a Qualification Status List (QSL) for use as Section 3 of the ALSEP Array D Acceptance Data Package (ADP).
  • 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.
  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1971)
    This ATM documents the Failure Modes, Effect and Criticality Analysis on the Bendix designed Power Conditioning Unit for the Array E ALSEP System. The analysis reflects analysis on those parts which are presently planned ...
  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1971)
    This ATM documents the Failure Modes, Effect and Criticality Analysis on the Bendix designed Power Conditioning Unit for the Array E ALSEP System. The analysis reflects analysis on those parts which are presently planned ...
  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1970)
    The purpose of the Failure Modes and Effects Analysis (FMEA) is to discover critical failure areas in the LRRR experiment and to remove susceptibility to such failures. Each possibility of failure is considered in light ...
  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1970)
    The major change between this document and corresponding documents as released by Gulton is the basic failure rate used in this ATM for the RCA CD4000 family of COS/MOS Fets. Bendix Reliability arrived at a more realistic ...
  • Baker, J. T.; Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1971)
    In compliance with NASA Contract NASA 9-5829 requirements, this document provides a Qualification Status List (QSL) for use as part of the ALSEP Flight 2A Acceptance Data Package.
  • Staats, J. T.; Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1971)
    This document provides a Qualification Status List (QSL) for use as part of the ALSEP Fuel Cask and Structure Assembly Flight 6 Acceptance Data Package (ADP). As of the date of publication, the information contained herein ...
  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1970)
    Releases the Failure Mode Summary into the Bendix documentation system for the Resettable Solid State Timer. The basic failure rates for the parts covered by this document were taken from ATM 879 which is the Failure Modes ...
  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1970)
    The major change between this document and corresponding documents as released by Gulton is the basic failure rate used in this ATM for the RCA CD4000 family of COS/MOS Fets. Bendix Reliability arrived at a more realistic ...
  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1970)
    The failure rates are listed on reliability worksheets and were adjusted for temperature and stress ratios, and screening reduction factors. The numerical reliability prediction for the RSST two year lunar phase of operation ...

Search HOU Repository

Browse

My Account