• DocumentCode
    3204854
  • Title

    Memory technologies and data recorder design

  • Author

    Strauss, Karl F.

  • Author_Institution
    Jet Propulsion Lab., Pasadena, CA
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    18
  • Abstract
    Missions, both near Earth and deep space, are under consideration that will require data recorder capacities of such magnitude as to be unthinkable just a few years ago. Concepts requiring well over 16,000 GB of storage are being studied. To achieve this capacity via ldquonormal meansrdquo was considered incredible as recently as 2004. This paper is presented in two parts. Part I describes the analysis of data recorder capacities for missions as far back as 35 years and provides a projection of data capacities required 20 years from now based upon missions either nearing launch, or in the planning stage. The paper presents a similar projection of memory device capacities as baselined in the ITRS - the International Technology Roadmap for Semiconductors. Using known Total Ionizing Dose tolerance going back as far as a decade, a projection of total dose tolerance is made for two prime technologies out to the year 2028. Based upon the two prime technologies, the design of a 130 Tb recorder is discussed in Part II. Further, it is noted that, for all the missions and technologies analyzed, the parameters of a recorder - mass, power, volume - remain constant despite ever-increasing capacity requirements.
  • Keywords
    aerospace instrumentation; data recording; digital storage; data capacities; data recorder design; memory device capacities; memory technologies; total ionizing dose tolerance; Belts; Capacity planning; Earth; History; Moon; Semiconductor device manufacture; Solid state circuits; Space missions; Space technology; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace conference, 2009 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4244-2621-8
  • Electronic_ISBN
    978-1-4244-2622-5
  • Type

    conf

  • DOI
    10.1109/AERO.2009.4839509
  • Filename
    4839509