Abstract. We present the high-frequency properties of the eight electric field sensors as proposed to be launched on the spacecraft "RESONANCE" in the near future. Due to the close proximity of the conducting spacecraft body, the sensors (antennas) have complex receiving features and need to be well understood for an optimal mission and spacecraft design. An optimal configuration and precise understanding of the sensor and antenna characteristics is also vital for the proper performance of spaceborne scientific instrumentation and the corresponding data analysis. The provided results are particularly interesting with regard to the planned mutual impedance experiment for measuring plasma parameters. Our computational results describe the extreme dependency of the sensor system with regard to wave incident direction and frequency, and provides the full description of the sensor system as a multi-port scatterer. In particular, goniopolarimetry techniques like polarization analysis and direction finding depend crucially on the presented antenna characteristics.
The RESONANCE projectThe RESONANCE project is dedicated to the investigation of properties and features of Earth's auroral acceleration zone as well as near-equatorial phenomena. The missions overarching goal is to study wave-particle interactions in the inner magnetosphere. Features to be observed include the energy transfer between energetic particle species, particle precipitation, the magnetospheric cyclotron maser and the generation of planetary radio emissions (Demekhov et al., 2003) such as the auroral kilometric radiation. Comprised of four satellites and flying a magneto-synchronous formation, the mission seems ideal for the investigation of effects and processes which are occurring along the geomagnetic flux tubes. Of particular interest is the energy exchange between the ionospheric and magnetospheric layers of Earth's atmosphere. Compared to previous radio science missions (cf. Table 1;Boudjada et al., 2010), RESONANCE provides the unique feature of sampling the same physical parameters in two space regions belonging to the same magnetic flux tube. The mission features, as well as the proposed spacecraft design, have already been described in Mogilevsky et al. (2002Mogilevsky et al. ( , 2013.The measurement of electric field parameters in spaceborne radio astronomy poses a substantial challenge, since the observed values range from several Hz to several 10s of MHz (in case of RESONANCE 10 MHz) and often comprises a large dynamic range. Gurnett (1998) provided a good overview and showed the large range that instruments usually have to cover in frequency, power, time and spatial scale. This is caused not only by the desire of the mission planers for acquiring a maximized data set, spanning as many phenomena as possible, but also by the fact that the satellite trajectories often pass through regions of different ambient conditions.Published by Copernicus Publications on behalf of the European Geosciences Union.