Unusual locations of Earth's bow shock on September 24 - 25, 1987: Mach number effects

Details Unusual locations of Earth's bow shock on September 24 - 25, 1987: Mach number effects Unusual locations of Earth's bow shock on September 24 - 25, 1987: Mach number effects

Jan 1995

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1995jgr...100...47c&link_type=abstract

Journal of Geophysical Research (ISSN 0148-0227), vol. 100, no. A1, p. 47-62

Other

42

Mach Number, Magnetopause, Position (Location), Shapes, Shock Waves, Solar Wind, Explorer 50 Satellite, International Sun Earth Explorers, Mathematical Models

Scientific paper

International Sun Earth Explorer 1 (ISEE 1) and Interplanetary Monitoring Platform 8 (IMP 8) data are used to identify 19 crossings of Earth's bow shock during a 30-hour period following 0000 UT on September 24, 1987. Apparent standoff distances for the shock are calculated for each crossing using two methods and the spacecraft location; one method assumes the average shock shape, while the other assumes a ram pressure-dependent shock shape. The shock's apparent standoff distance, normally approximately 14 R(sub E), is shown to increase from near 10 R(sub E) initially to near 19 R(sub E) during an 8-hour period, followed by an excursion to near 35 R(sub E) (where two IMP 8 shock crossings occur) and an eventual return to values smaller than 19 R(sub E). The Alfven M(sub A) and fast magnetosonic M(sub ms). Mach numbers remain above 2 and the number density above 4/cu cm for almost the entire period. Ram pressure effects produce the initial near-Earth shock location, whereas expansions and contractions of the bow shock due to low Mach number effects account, qualitatively and semiquantitatively, for the timing and existence of almost all the remaining ISEE crossings and both IMP 8 crossings. Significant quantitative differences exist between the apparent standoff distances for the shock crossings and those predicted using the observed plasma parameters and the standard model based on Spreiter et al.'s (1966) gasdynamic equation. These differences can be explained in terms of either a different dependence of the standoff distance on Mach number at low M(sub A) and M(sub ms), or variations in shock shape with M(sub A) and M(sub ms) (becoming increasingly "puffed up" with decreasing M(sub A) and M(sub ms), as expected theoretically), or by a combination of both effects.

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