Energetic positive and negative cloud‐to‐ground (CG) flashes are both capable of producing sprites. Negative CGs typically outnumber the positive ones by 10 to 1. However, >99.9 % of reported sprites were found to be initiated by positive CGs—thus the polarity paradox. Here, sprites recorded by the Imager of Sprites and Upper Atmospheric Lightning (ISUAL) mission were analyzed along with extremely low‐frequency band magnetic field data to resolve this paradox. Approximately twenty‐five percent of the sprites are found to be associated with negative CG lightning. “Negative” sprites mainly congregate in the latitudinal regions below 20°, while positive sprites scatter up to 50°. The ISUAL negative sprites are evidently beyond the observable ranges of the ground sites reported in previous studies. Hence, the sprite polarity paradox is likely a selection effect of the middle‐ to high‐altitudinal observation sites. The charge moment changes and accompanying transient luminous events of sprites were also examined and found to be polarity dependent.

Precaution to remove the serious effect of electrode contamination in Langmuir probe experiments has not been taken in many space measurements because the effect is either not understood or ignored. We stress here that one should pay extra attention to the electrode contamination effect to get accurate and reliable plasma measurements so that the long time effort for sounding rocket/satellite missions does not end in vain or becomes less fruitful. In this paper, we describe two main features of voltage-current characteristic curves associated with the contaminated Langmuir probe, which are predicted from the equivalent circuit model, which we proposed in 1970's. We then show that fast sweeping dc Langmuir probes can give reliable results in the steady state regime. The fast sweeping probe can also give reliable results in transient situations such as satellite moves through plasma bubble in the ionosphere where the electron density drastically changes. This fact was first confirmed in our laboratory experiment.

The DC Langmuir probe is a widely-used instrument for the plasma measurement in the space missions. But to apply DC Langmuir probe to a tiny satellite, such as a cubesat, for ionosphere study is difficult to get accurate electron density (ne) and electron temperature (Te) for two reasons: the contamination on both satellite surface and the electrode to be used, and a lack of conductive surface area of the tiny satellite. Under the charging effect of the satellite with an insufficient area ratio between the surface of the probe and the spacecraft, the contaminations on the surface of both probe and the satellite, acting as equivalent capacitances and resistances, modify both the potentials on the satellite and the probe, and an elevated Te and a suppressed ne are derived incorrectly. In this paper, the effect of the surface contamination on the DC Langmuir probe measurements onboard a tiny satellite is investigated in detail. The effects of the accumulated charge and the impedances on the contamination layers have been identified in the experiments done in a ground chamber with similar plasma conditions in the Earth’s ionosphere, and the characteristic dependences of the probe sweeping frequency and the plasma density are presented. The experiment result suggests that a contamination-free instrument TeNeP, operated at 0.2∼10 MHz probe sweeping frequency and sweeping potentials below 500 mV, is a better solution to obtain accurate Te and ne, onboard a satellite with a surface area ratio below 100.

Problems associated with Retarding Potential Analyzer (RPA), which can be used to measure ion temperature/and density in the lower E region where ion temperature is 200-300 K, are discussed. Two major factors which need to be taken care of to get accurate ion temperature of extremely low values are the effect of mesh size of the grids to be used and the effect of electrode contamination. An electrode baking and vacuum sealing mechanisms are designed to keep the electrode surface clean. The effect of mesh sizes on the calculation of ion temperature is discussed by using simulation studies as well as laboratory experiments. The study suggests that the uniformity of the electric field in the RPA sensor is critical. The manuscript describes the principle of the RPA, the effect of the mesh size using computer simulation studies, and the mechanical design of the sensor sealing to remove electrode contamination.

A compact and low power consumption instrument for measuring the electron density and temperature in the ionosphere has been developed by modifying the previously developed Electron Temperature Probe (ETP). A circuit block which controls frequency of the sinusoidal signal is added to the ETP so that the instrument can measure both T(e) in low frequency mode and N(e) in high frequency mode from the floating potential shift of the electrode. The floating potential shift shows a minimum at the upper hybrid resonance frequency (f(UHR)). The instrument which is named "TeNeP" can be used for tiny satellites which do not have enough conductive surface area for conventional DC Langmuir probe measurements. The instrument also eliminates the serious problems associated with the contamination of satellite surface as well as the sensor electrode.