标题:Wire Probe Antenna (WPT) and Electric Field Detector (EFD) of Plasma Wave Experiment (PWE) aboard the Arase satellite: specifications and initial evaluation results
摘要:This paper summarizes the specifcations and initial evaluation results of Wire Probe Antenna (WPT) and Electric Field
Detector (EFD), the key components for the electric feld measurement of the Plasma Wave Experiment (PWE) aboard
the Arase (ERG) satellite. WPT consists of two pairs of dipole antennas with ~ 31-m tip-to-tip length. Each antenna element has a spherical probe (60 mm diameter) at each end of the wire (15 m length). They are extended orthogonally
in the spin plane of the spacecraft, which is roughly perpendicular to the Sun and enables to measure the electric
feld in the frequency range of DC to 10 MHz. This system is almost identical to the WPT of Plasma Wave Investigation aboard the BepiColombo Mercury Magnetospheric Orbiter, except for the material of the spherical probe (ERG:
Al alloy, MMO: Ti alloy). EFD is a part of the EWO (EFD/WFC/OFA) receiver and measures the 2-ch electric feld at a
sampling rate of 512 Hz (dynamic range: ± 200 mV/m) and the 4-ch spacecraft potential at a sampling rate of 128 Hz
(dynamic range: ± 100 V and ± 3 V/m), with the bias control capability of WPT. The electric feld waveform provides
(1) fundamental information about the plasma dynamics and accelerations and (2) the characteristics of MHD and
ion waves in various magnetospheric statuses with the magnetic feld measured by MGF and PWE–MSC. The spacecraft potential provides information on thermal electron plasma variations and structure combined with the electron
density obtained from the upper hybrid resonance frequency provided by PWE–HFA. EFD has two data modes. The
continuous (medium-mode) data are provided as (1) 2-ch waveforms at 64 Hz (in apoapsis mode, L > 4) or 256 Hz
(in periapsis mode, L < 4), (2) 1-ch spectrum within 1–232 Hz with 1-s resolution, and (3) 4-ch spacecraft potential at
8 Hz. The burst (high-mode) data are intermittently obtained as (4) 2-ch waveforms at 512 Hz and (5) 4-ch spacecraft
potential at 128 Hz and downloaded with the WFC-E/B datasets after the selection. This paper also shows the initial
evaluation results in the initial observation phase.
关键词:Electric field; Plasma wave; Spacecraft potential; Electron density and temperature; Wire Probe Antenna (WPT); Electric Field Detector (EFD); Plasma Wave Experiment (PWE); Arase spacecraft