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The Interaction of the Solar Wind with Solar Probe Plus - 3D Hybrid Simulation: The Study for the Distance 4.5Rs - Report 1Our report devotes a 3D numerical hybrid model of the interaction of the solar wind with the Solar Probe spacecraft. The SPP model includes 3 main parts, namely, a non-conducting heat shield, a support system, and cylindrical section or spacecraft bus that contains the particle analysis devices and antenna. One observes an excitation of the low frequency Alfven and whistler type wave directed by the magnetic field with an amplitude of about (0.06-0.6) V/m. The compression waves and the jumps in an electric field with an amplitude of about (0.15-0.7) V/m were also observed. The wave amplitudes are comparable to or greater than previously estimated max wave amplitudes that SPP is expected to measure. The results of our hybrid simulation will be useful for understanding the plasma environment near the SPP spacecraft at the distance 4.5 Rs. Future simulation will take into account the charging of the spacecraft, the charge separation effects, an outgassing from heat shield, a photoionization and an electron impact ionization effects near the spacecraft.
Document ID
20110004138
Acquisition Source
Goddard Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Lipatov, Alexander S.
(Maryland Univ. Baltimore County Baltimore, MD, United States)
Sittler, Edward C.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Hartle, Richard E.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Cooper, John F.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 25, 2013
Publication Date
December 1, 2010
Subject Category
Plasma Physics
Report/Patent Number
Rept-2011-00670
NASA/TM-2010-215862/REPT1
Report Number: Rept-2011-00670
Report Number: NASA/TM-2010-215862/REPT1
Funding Number(s)
CONTRACT_GRANT: NCC5-494
WBS: WBS 93672302010619
CONTRACT_GRANT: 93672302010619
Distribution Limits
Public
Copyright
Public Use Permitted.
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