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‡a(MiU)990161180560106381
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‡asdr-miu.990161180560106381
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‡aMAIN
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‡aD 301.45/39:959
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‡aADA 176881
|
088 |
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‡aAFGL TR 86-160
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100 |
1 |
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‡aHeinemann, M.
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245 |
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‡aComputer models of the spacecraft wake /
‡cM. Heinemann, A. Rubin, M. Tautz, D. Cooke.
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1 |
‡aHanscom AFB, Massachusetts :
‡bAir Force Geophysics Laboratory, Air Force Systems Command, United States Air Force,
‡c1986.
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‡avi, 23 pages :
‡billustrations ;
‡c28 cm.
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‡atext
‡btxt
‡2rdacontent
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‡aunmediated
‡bn
‡2rdamedia
|
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‡avolume
‡bnc
‡2rdacarrier
|
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‡aEnvironmental Research Papers ;
‡vNo. 959
|
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0 |
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‡aAFGL TR ;
‡v86-160
|
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⊔ |
‡aResearch supported by the Air Force Geophysics Laboratory, United States Air Force, Hanscom AFB, Massachusetts.
|
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‡aSpace Physics Division Project 7601.
|
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‡aOther authors listed on title page
|
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‡aADA176881 (from http://www.dtic.mil).
|
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‡a"24 July 1986."
|
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‡aIncludes bibliographical references (page 23).
|
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‡aCalculations of the spacecraft interaction with the low earth orbit space plasma environment are presented, based on two computer codes, MACH and POLAR. MACH is an inside-out particle tracking code which treats spacecraft in a cylindrically symmetric grid, while POLAR is fully three dimensional. The methodology of MACH is more fundamental than that of POLAR, and MACH is used for validating the physics of POLAR in regimes where there are no comprehensive theoretical of experimental results. POLAR and MACH solutions for the wake of a charged disk in MACH 4, 5, and 8 flow are compared.
|
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‡aMode of access: Internet.
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‡aIons
‡xDensity.
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0 |
‡aComputer programs.
|
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0 |
‡aPlasma sheaths.
|
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‡aFluid dynamics (Space environment)
‡xMathematical models.
|
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1 |
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‡aCooke, D.
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1 |
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‡aTautz, M.
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1 |
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‡aRubin, A.
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‡aU.S. Air Force Geophysics Laboratory.
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‡aTechnical Report Archive & Image Library (TRAIL)
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‡a39015095141035
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