Computer Science – Sound
Scientific paper
Aug 2001
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2001esasp.471..363h&link_type=abstract
In: 15th ESA Symposium on European Rocket and Balloon Programmes and Related Research, 28 - 31 May 2001, Biarritz, France. Ed.:
Computer Science
Sound
Earth Ionosphere, Spread-F, Langmuir Probe, Impedance Probe
Scientific paper
In the DEOS project three sounding rockets (F05-F07) were launched from SHAR, South India into the equatorial ionosphere in April and September 1998. In order to study the dynamics of the E-and F-region at the edge of the equatorial electrojet, and make in-situ measurements in a ionosphere perturbed by equatorial Spread-F, each payload was equipped with an Impedance probe (IP), two Langmuir probes in fluctuation (LP2) and swept mode (LP1), a resonance cone instrument (RC) and a radio beacon experiment (RABER). This payload allowed to make absolute measurements of the electron temperature Te, the electron density ne, density fluctuations δne/ne and the total electron content TEC at altitudes up to 430 km. On the upleg of flight F06, density depletions below the F-maximum were observed by the IP and LP instruments, whereas on the downleg a smooth density profile was encountered. Density profiles from both instruments are compared in perturbed and unperturbed conditions and show a close agreement. Profiles from flights F05 and F07 are also presented. The in-situ electron density profiles are compared with ground based measurements. Profiles of the absolute electron temperature measured by the LP1 during flight F06 show a reduced electron temperature inside the density depletions.
Hirt Markus
Mayer Gerhard
Piel Alexander
Steigies Christian T.
Thiemann Heinz
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