TARANIS

Mission type| Magnetosphere,
ionosphere and
atmosphere studies
Operator| Centre national d'études spatiales (CNES)
Website| https://taranis.cnes.fr
Mission duration| 4 years (planned) [1]
Spacecraft properties
Bus| Myriade
Manufacturer| Centre national d'études spatiales (CNES)
Launch mass| 175 kg
Power| 85 watts
Start of mission
Launch date| 17 November 2020,
01:52:20 UTC
Rocket| Vega VV17
Launch site| Centre Spatial Guyanais, ELV
Contractor| Avio, Italy
End of mission
Decay date| Launch failure (4th stage)
Cause: human error
Last contact: November 17, 2020
Did not achieve orbit, so decay was imminent[2]
Orbital parameters
Reference system| Geocentric orbit
Regime| Sun-synchronous orbit
Altitude| 676.0 km
Inclination| 98.19°

TARANIS (Tool for the Analysis of Radiation from lightning and Sprites) was an observation satellite of the French Space Agency (CNES) which would have studied the transient events produced in the Earth's atmospheric layer between 10 km (6.2 mi) and 100 km (62 mi) altitude.[3][4] 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.

## Contents

* 1 Science objectives
* 2 Technical characteristics
* 3 Flight
* 3.1 Launch failure
* 4 Replacement
* 5 See also
* 6 References

## Science objectives

The satellite was intended to collect data on transient events that are observed during thunderstorms.[5] These events happen between the medium and upper atmosphere, the ionosphere and the magnetosphere (radiation belts). The resulting phenomena in visible light are called Transient Luminous Events (TLE) 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 (TGF), generated by intense electric fields in which the electrons are accelerated to the point of reaching energies up to 40 MeV (the bremsstrahlung process produces the photons). The link between TLEs and TGFs was one of the scientific questions of the TARANIS mission.[5] The Lightning induced electron precipitation (LEP) were also to be studied.[5] All these events have associated electromagnetic wave emissions which also had to be studied.[5]

The Atmosphere-Space Interactions Monitor (ASIM) 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:[6]

* MCP (MicroCameras and Photometers),[7] 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 (X-ray, Gamma-ray and Relativistic Electrons),[8][9] set of three detectors to measure high energy photons (1 MeV to 10 MeV).
* IDEE (Instruments for the Detection of high-Energy Electrons),[10][9] 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 (Institut de recherche en astrophysique et planétologie) astrophysics and planetology research institute.
* IME-BF,[11] low frequency antenna to measure the electric field to a frequency up to 3.3 MHz.
* IME-HF,[12] high frequency antenna to measure the electric field at frequencies of 100 kHz to 30 MHz.
* IMM,[13] a tri-axis magnetometer of « search-coil » type to measure the magnetic field.
* MEXIC (MultiEXperiment Interface Controller).[14]

The studied phenomena last not more than a few milliseconds (except blue jets), therefore a specific recording method is implemented. Scientific instruments operate continuously and data is stored in a memory that is regularly purged of its oldest elements. If a phenomenon is noticed through one of the triggering instrument (XGRE, IDEE, MCP, IME-HF), the data of all the instruments corresponding to the period it took place is saved, and later transmitted to the ground.[8]

## Flight

After launch, TARANIS had to deploy instrument ramps and had to start several months of commissioning and validation. The scientific data were to be available from TARANIS in June 2021.[15] CNES has devoted around 115 million euros, or US136 million, to the TARANIS project since its start in 2010. The mission was designed to operate over two to four years.[15]

### Launch failure

TARANIS was launched from the Centre Spatial Guyanais at 01:52:20 UTC on 17 November 2020.[16] The flight was planned to deploy the satellites into 2 very slightly different sun-synchronous orbits at roughly 670 km (starting 54 minutes until 102 minutes after liftoff), before the upper stage would have re-ignited to re-enter the Earth's atmosphere.[1] However, the rocket failed after launch and the mission was lost. The exact cause could be first ignition of the engine of the Avum fourth stage, a deviation of trajectory was identified, entailing the loss of the mission.[5] Arianespace traces cause of Vega launch failure to "human error".[2] This was the Vega rocket's second failure in three missions.[17]

## Replacement

After TARANIS's failure to orbit, CNES started to plan a replacing mission TARANIS 2 in late 2020 and early 2021. TARANIS 2 is planned to achieve the same scientific objectives as TARANIS would have had TARANIS not failed.[18] TARANIS 2 is planned to launch around 2025.[19]

## See also

* French space program
* Guiana Space Centre

## References

1. ↑ 1.0 1.1 "Vega flight VV17 launch kit". Arianespace. November 2020. https://www.arianespace.com/wp-content/uploads/2020/11/VV17-launchkit-EN2.pdf.
2. ↑ 2.0 2.1 "Arianespace traces cause of Vega launch failure to "human error"". Spaceflight Now. 17 November 2020. https://spaceflightnow.com/2020/11/17/arianespace-traces-cause-of-vega-launch-failure-to-human-error/.
3. ↑ "Taranis". CNES. 24 April 2015. https://taranis.cnes.fr/en/TARANIS/index.htm.
4. ↑ Lefeuvre, Francois; Blanc, Elisabeth; Pinçon, Jean-Louis; Roussel-Dupré, Robert; Lawrence, David; Sauvaud, Jean-André; Rauch, Jean-Louis; Feraudy, Hervé de et al. (2008-06-01). "TARANIS—A Satellite Project Dedicated to the Physics of TLEs and TGFs". Space Science Reviews 137 (1–4): 301–315. doi:10.1007/s11214-008-9414-4. ISSN 0038-6308. Bibcode: 2008SSRv..137..301L. https://hal-insu.archives-ouvertes.fr/insu-02926960/file/lefeuvre.pdf.
5. ↑ 5.0 5.1 5.2 5.3 5.4 "Mission". 24 April 2015. https://taranis.cnes.fr/en/TARANIS/GP_mission.htm.
6. ↑ "Laboratoire de Physique et Chimie de l'Environnement et de l'Espace - TARANIS". CNES. http://www.lpc2e.cnrs.fr/spip.php?article171.
7. ↑ Farges, Thomas; Blanc, Elisabeth; Hébert, Philippe; Le Mer-Dachard, Fanny; Ravel, Karen; Gaillac, Stéphanie (2017-04-01). "MicroCameras and Photometers (MCP) on board TARANIS satellite". EGU General Assembly Conference Abstracts 19: 6024. Bibcode: 2017EGUGA..19.6024F.
8. ↑ 8.0 8.1 "TARANIS | LABORATOIRE". http://www.apc.univ-paris7.fr/APC_CS/en/taranis.
9. ↑ 9.0 9.1 Sarria, David; Lebrun, François; Blelly, Pierre-Louis; Chipaux, Rémi; Laurent, Philippe; Sauvaud, Jean-André; Prech, Lubomir; Devoto, Pierre et al. (2017-07-13). "TARANIS XGRE and IDEE detection capability of terrestrial gamma-ray flashes and associated electron beams". Geoscientific Instrumentation, Methods and Data Systems 6 (2): 239–256. doi:10.5194/gi-6-239-2017. ISSN 2193-0856. Bibcode: 2017GI......6..239S. https://www.geosci-instrum-method-data-syst.net/6/239/2017/.
10. ↑ VERT, Pole web service communication OMP. "TARANIS / Techniques et missions spatiales / La recherche / OMP". http://www.obs-mip.fr/recherche/techniques-missions-spatiales/projet-taranis.
11. ↑ ES. "Instrumentation". http://taranis.latmos.ipsl.fr/Instrumentation.html.
12. ↑ "TARANIS IME-HF | CZECH SPACE OFFICE". http://www.czechspace.cz/en/taranis-ime-hf.
13. ↑ "Laboratoire de Physique et Chimie de l'Environnement et de l'Espace". CNES. http://www.lpc2e.cnrs.fr/spip.php?article141.
14. ↑ "SATELLITE". CNES. 18 August 2016. https://taranis.cnes.fr/fr/TARANIS/Fr/GP_satellite.htm.
15. ↑ 15.0 15.1 "Vega rocket poised for launch with satellites for Spain and France". Spaceflight Now. 16 November 2020. https://spaceflightnow.com/2020/11/16/vega-rocket-poised-for-launch-with-satellites-for-spain-and-france/.
16. ↑ Clark, Stephen. "Live coverage: Arianespace probing "anomaly" shortly after Vega launch". Spaceflight Now. https://spaceflightnow.com/2020/11/16/vega-vv17-mission-status-center/.
17. ↑ "Status". NASASpaceflight.com. https://twitter.com/nasaspaceflight/status/1328536815117230080.
18. ↑ "Avio CEO promises Vega's rapid return to flight as CNES plots replacement satellite". 20 November 2020. https://spacenews.com/avio-ceo-promises-vegas-rapid-return-to-flight-as-cnes-plots-replacement-satellite/.
19. ↑ "Taranis 2". https://www.lpc2e.cnrs.fr/activites-scientifiques/plasmas-spatiaux/projets/missions-spatiales/taranis/.

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Orbital launches in 2020

January|

* Starlink 2 (60 satellites)
* TJSW-5
* Jilin-1 Kuanfu-01, ÑuSat 7, 8, Tianqi-5
* Yinhe-1 / GS-SparkSat-03 / Galaxy-1
* Eutelsat Konnect, GSAT-30
* Starlink 3 (60 satellites)
* NROL-151

February|

* OneWeb × 34
* IGS-Optical 7
* Zafar 1†
* Solar Orbiter
* Cygnus NG-13
* Starlink 4 (60 satellites)
* JCSAT-17, GEO-KOMPSAT-2B
* XJS-C, D, E, F
* Meridian-M 9

March|

* SpaceX CRS-20
* BeiDou-3 G2Q
* Xinjishu Yanzheng-6
* GLONASS-M 760
* Starlink 5 (60 satellites)
* OneWeb × 34
* Yaogan 30-06 01, 02, 03
* AEHF-6

April|

* Soyuz MS-16
* Nusantara Dua†
* Noor
* Starlink 6 (60 satellites)
* Progress MS-14

May|

* Chinese next-generation crewed spacecraft / Flexible Inflatable Cargo Return Module
* Xingyun-2 01, 02
* X-37B OTV-6 / FalconSAT-8
* HTV-9
* EKS-4
* LauncherOne†,
* Starshine 4†
* XJS-G, XJS-H
* Crew Dragon Demo-2

June|

* Starlink 7 (60 satellites)
* Starlink 8 (58 satellites)

July|

* Progress MS-15

August|

* Starlink 9 (57 satellites)
* Starlink 10 (58 satellites)

September|

* Vega VV16 (65 satellites)
* Starlink 11 (60 satellites)

October|

* Cygnus NG-14
* Soyuz MS-17
* Starlink 12 (60 satellites)
* Starlink 13 (60 satellites)
* Starlink 14 (60 satellites)

November|

* SpaceX Crew-1
* Chang'e 5
* Vega VV17†,
* SEOSat-Ingenio†, TARANIS†
* Starlink 15 (60 satellites)

December|

* SpaceX CRS-21

Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Cubesats are smaller.
Crewed flights are bolded. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in brackets).

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