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Sunday, August 22, 2021 | History

3 edition of Fesibility of self-structured current accessed bubble devices in spacecraft recording systems found in the catalog.

Fesibility of self-structured current accessed bubble devices in spacecraft recording systems

Fesibility of self-structured current accessed bubble devices in spacecraft recording systems

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  • 24 Currently reading

Published by Sperry Corporation, National Aeronautics and Space Administration, Langley Research Center in St. Paul, Mn, Hampton, Va .
Written in English

    Subjects:
  • Magnetic bubble devices.,
  • Airborne/spaceborne computers.,
  • Architecture (computers),
  • Bubble memory devices.

  • Edition Notes

    Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1985. 3 microfiches.

    StatementG.L. Nelson, D.R. Krahn.
    SeriesNASA contractor report -- 172554., NASA contractor report -- NASA CR-172554.
    ContributionsKrahn, Donald Robert, 1948-, Sperry Corporation., Langley Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL16157030M


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Fesibility of self-structured current accessed bubble devices in spacecraft recording systems Download PDF EPUB FB2

Feasibility of self-structured current accessed bubble devices in spacecraft recording systems The self-structured, current aperture approach to Author: G. Nelson, D. Krahn, R. Dean, M. Paul, D. Lo, D. Amundsen, G. Stein. The self-structured, current aperture approach to magnetic bubble memory is described.

Key results include: (1) demonstration that self-structured bubbles (a Author: G. Nelson, D. Krahn, R. Dean, M. Paul, D. Lo, D. Amundsen, G. Stein. develop the next generation of spacecraft to transport cargo, equipment, and human explorers to space. These vehicles are part of the Constellation Program, which is.

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The current state of bubble memory technology is reviewed in terms of memory element, memory element packaging and system design with special attention to those Author: G. Murray. average value of current due to the integral over angle for non-normal incidence. If the flux is not isotropic, these simple calculations must be redone for the actual.

E2_Spacecraft_Structures_C3 Aerospace Education Services Project 3 The Significance of Mass: Every pound that is carried to space requires fuel to do so, regardless. Spacecraft mechanical environment 3.

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