Figure 4


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Detrended ne (a, b), PSD of the m-NLP ne fluctuations with the spectral break frequency (c, d), LF ad HF slopes of the corresponding PSD (e, f), integrated power from the PSD for frequency intervals of 10 Hz (g, h) and for intervals of 100 Hz (i, j), electron precipitation measured with the EEPAA (k, l) E × B-drift velocity vD in ENU-coordinates (m, n) of the high flyer and low flyer, respectively. The transparent data intervals correspond to attitude changes of the spacecraft. The x-axes correspond to UT (upper line), the magnetic footprint of the spacecraft (middle line), and the altitude of the rocket (bottom line).

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