DocumentCode
1043098
Title
Electron densities of the ionosphere utilizing high-altitude rockets
Author
Haycock, O.C. ; Swigart, J.I. ; Baker, D.J.
Author_Institution
University of Utah, Salt Lake City, UT, USA
Volume
7
Issue
4
fYear
1959
fDate
10/1/1959 12:00:00 AM
Firstpage
414
Lastpage
418
Abstract
The problem of determining the electron densities in the
-region of the ionosphere is approached by using 6-mc pulse transmissions from a rocket to several ground receiving stations. A logical and complete development, using dyadic techniques, is given for obtaining the propagation constant of the dissipative, anisotropic ionosphere. Special cases of the magneto-ionic formulas are given, and comparison of the ionosphere with a distributed-constant transmission line is made. In a nondissipative ionosphere, formulas are developed establishing the relationship between the effective electron density and the relative transmission delay of the 6-mc pulse. A description of the University of Utah\´s vertical incidence experiment is given in which a 6-mc pulse from an airborne transmitter is received simultaneously at several ground receiving stations. The relative 6-mc time-delay data from three Aerobee high-altitude rockets launched from Holloman Air Development Center on July 1, 1953, November 3, 1953, and June 13, 1956, were obtained and, from these, electron density was calculated. Curves showing the profile of electron density as a function of altitude as calculated both during the rocket ascent and descent are presented. The curves indicate a general increase of electron density throughout the
- region, rising from nearly zero at 85 km to a maximum of about
electrons/m3. The maximum altitude attained by the rockets allowed exploration up to 137 km above sea level.
-region of the ionosphere is approached by using 6-mc pulse transmissions from a rocket to several ground receiving stations. A logical and complete development, using dyadic techniques, is given for obtaining the propagation constant of the dissipative, anisotropic ionosphere. Special cases of the magneto-ionic formulas are given, and comparison of the ionosphere with a distributed-constant transmission line is made. In a nondissipative ionosphere, formulas are developed establishing the relationship between the effective electron density and the relative transmission delay of the 6-mc pulse. A description of the University of Utah\´s vertical incidence experiment is given in which a 6-mc pulse from an airborne transmitter is received simultaneously at several ground receiving stations. The relative 6-mc time-delay data from three Aerobee high-altitude rockets launched from Holloman Air Development Center on July 1, 1953, November 3, 1953, and June 13, 1956, were obtained and, from these, electron density was calculated. Curves showing the profile of electron density as a function of altitude as calculated both during the rocket ascent and descent are presented. The curves indicate a general increase of electron density throughout the
- region, rising from nearly zero at 85 km to a maximum of about
electrons/m3. The maximum altitude attained by the rockets allowed exploration up to 137 km above sea level.Keywords
Ionospheric measurements; Microwave radio propagation; Anisotropic magnetoresistance; Delay effects; Electrons; Ionosphere; Magnetic anisotropy; Perpendicular magnetic anisotropy; Propagation constant; Rockets; Transmission lines; Transmitters;
fLanguage
English
Journal_Title
Antennas and Propagation, IRE Transactions on
Publisher
ieee
ISSN
0096-1973
Type
jour
DOI
10.1109/TAP.1959.1144691
Filename
1144691
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