Large Satellite Bus ReliabilityNASA is proposing to build a small space station in Cis-lunar orbit called Deep Space Gateway (DSG). At the heart of the DSG is the Power and Propulsion Element (PPE) which is conceptually similar to previously designed and operated satellite buses. A satellite bus is composed of the satellite spacecraft infrastructure minus the payload, and generally includes power, propulsion, avionics, and guidance, navigation and control. In November of 2017, five companies were awarded contracts by NASA to research PPE designs. In order to better understand the reliability of large satellite buses which may be the starting point of the PPE, NASA used Weibull analysis to evaluate spacecraft with similar masses and design life to the PPE. In addition, a subset of the large satellites which had satellite buses manufactured by any one of the five companies was also evaluated. This paper provides the results of the reliability analysis and compares the reliability of the general population of large satellites to the reliability associated with large satellite buses manufactured by the five companies currently studying PPE options.
Document ID
20180006794
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Hamlin, Teri L. (NASA Johnson Space Center Houston, TX, United States)
Reistle, Bruce C. (NASA Johnson Space Center Houston, TX, United States)
Stewart, Michael A. (NASA Johnson Space Center Houston, TX, United States)
Date Acquired
October 24, 2018
Publication Date
September 16, 2018
Subject Category
Spacecraft Design, Testing And PerformanceQuality Assurance And Reliability
Report/Patent Number
JSC-E-DAA-TN57726Report Number: JSC-E-DAA-TN57726
Meeting Information
Meeting: Probabilistic Safety Assessment and Management 14