Rocket Instruments
- S-310-44 The following experiments were carried out.
- Plasma Wave Monitor (PWM)
In order to understand electron heating phenomena around Sq current focus, plasma waves associated with them are measured by the receiver in a frequency range from 300 Hz to 22 MHz using antenna of Electric Field Detector (EFD) with a tip-to-tip length of 2 m.
- Tracking Data
Latitude, longitude, and height of the sounding rocket as a function of X, time from the launch. The data file is provided in the Microsoft Excel format. - S-520-26 The following experiments were carried out.
- Number density measurement of Electron by Impedance probe (NEI)
In order to understand interactions of ionized and neutral atmosphere in ionospheric E and F regions, electron number density in a range from 10^3 to 2x10^6 /cc is measured along the rocket trajectory by impedance probe.
- Plasma Wave Monitor (PWM)
In order to understand interactions of ionized and neutral atmosphere in ionospheric E and F regions, plasma waves associated with them are measured by the receiver in a frequency range from 300 Hz to 22 MHz using antenna of Electric Field Detector (EFD).
- Tracking Data
Latitude, longitude, and height of the sounding rocket as a function of X, time from the launch. The data file is provided in the text format. - S-520-27 The following experiments were carried out.
- Number density measurement of Electron by Impedance probe (NEI)
In order to understand the plasma structures in the ionosphere during the interaction processes between E and F regions, electron number density in a range from 10^3 to 2x10^6 /cc is measured along the rocket trajectory by impedance probe.
- Tracking Data
Latitude, longitude, and height of the sounding rocket as a function of X, time from the launch. The data file is provided in the Microsoft Excel format. - S-520-29 The following experiments were carried out.
- Number density measurement of Electron by Impedance probe (NEI)
In order to measure the vertical structure of the sporadic E layers, electron number density in a range from 10^3 to 2x10^6 /cc is measured along the rocket trajectory by impedance probe.
- Tracking Data
Latitude, longitude, and height of the sounding rocket as a function of X, time from the launch. The data file is provided in the text format.