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‡a(MiU)990161180450106381
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‡aD 301.45/39:945
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‡aADA 172276
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‡aAFGL TR 86-23
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1 |
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‡aHeinemann, Michael.
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‡aShuttle contamination modeling :
‡bEvolution of ionized shuttle exhaust /
‡cMichael Heinemann.
|
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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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‡aiii, 27 pages :
‡billustrations ;
‡c28 cm.
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‡atext
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‡aEnvironmental Research Papers ;
‡vNo. 945
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‡aAFGL TR ;
‡v86-23
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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 7661.
|
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‡aADA172276 (from http://www.dtic.mi).
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‡a"22 January 1986."
|
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‡aIncludes bibliographical references (page 27).
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‡aWe consider the evolution of ionized Shuttle exhaust. While the source of ionization is not treated, the subsequent evolution can be understood in a certain amount of detail. The fundamental conclusion are that: (1) Low-density ions expand with neutral exhaust for about 100 m where they go through a rapid transition to collisionless behavior and then are swept away (in the Shuttle frame of reference) by the magnetic field, and radially away from the Shuttle: neither the ambient ionosphere nor the geomagnetic field can significantly change this behavior. The details of the evolution can be affected by low-level (approx. 0.1 mV/m) parallel electric fields. The mirror force associated with the geomagnetic field is to weak to have any effect.
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‡aMode of access: Internet.
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‡aSpace vehicles
‡xContamination
‡xMathematical models.
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‡aSpace environment.
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‡aMagnetic fields.
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‡aGeomagnetism.
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‡aMagnetic fields.
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‡aGeomagnetism.
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⊔ |
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‡aSpace vehicles
‡xContamination
‡xMathematical models.
|
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⊔ |
0 |
‡aSpace environment.
|
650 |
⊔ |
0 |
‡aSpace plasmas.
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‡aU.S. Air Force Geophysics Laboratory.
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‡aTechnical Report Archive & Image Library (TRAIL)
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