TARANIS
TARANIS was an observation satellite of the French Space Agency which would have studied the transient events produced in the Earth's atmospheric layer between and altitude. TARANIS was launched in November 2020 with SEOSat-Ingenio aboard Vega flight VV17 and would have been placed in a Sun-synchronous orbit at an altitude of 676 km, for a mission duration of two to four years, but the rocket failed shortly after launch.
Science objectives
The satellite was intended to collect data on transient events that are observed during thunderstorms. These events happen between the medium and upper atmosphere, the ionosphere and the magnetosphere. The resulting phenomena in visible light are called Transient Luminous Events and take a great diversity of forms sprites, blue jets, red giants, halos, elves, varying in color, shape and duration, and relations between them. Thunderstorms are also known to generate gamma and X-ray photon emissions called Terrestrial Gamma-ray Flashes, generated by intense electric fields in which the electrons are accelerated to the point of reaching energies up to 40 MeV. The link between TLEs and TGFs was one of the scientific questions of the TARANIS mission. The Lightning induced electron precipitation were also to be studied. All these events have associated electromagnetic wave emissions which also had to be studied.The Atmosphere-Space Interactions Monitor of the International Space Station was to operate concurrently with TARANIS and was to provide additional observations.
Technical characteristics
The TARANIS microsatellite had a mass of 175 kg, and used the Myriade platform powered by solar panels providing 85 watts. The amount of data transferred should have been 24 Gigabits per day. The scientific payload was made of seven instruments:- MCP, set of two cameras and three photometers, 30 frames/s, 512 x 512 pixels and measuring the luminance in several spectral bands at high resolution.
- XGRE, set of three detectors to measure high energy photons.
- IDEE, set of two electron detectors to measure their spectrum between 70 keV to 4 MeV together with their pitch angle. The sensors were developed by the IRAP astrophysics and planetology research institute.
- IME-BF, low frequency antenna to measure the electric field to a frequency up to 3.3 MHz.
- IME-HF, high frequency antenna to measure the electric field at frequencies of 100 kHz to 30 MHz.
- IMM, a tri-axis magnetometer of « search-coil » type to measure the magnetic field.
- MEXIC.