HENON

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HENON
Mission type Space weather probe
Operator ESA
Spacecraft properties
Spacecraft type12U CubeSat
Manufacturer Argotec
Start of mission
Launch dateNET 2026
  GOMX-5

HENON (HEliospheric pioNeer for sOlar and interplanetary threats defeNce), is a planned space weather and technology demonstration mission by the European Space Agency (ESA) in the form of a 12U CubeSat. [1] It will be ESA's first stand-alone deep space CubeSat. The goal of the mission is to demonstrate solar storm forecasting capabilities with 3–6 hours of advance warning before a storm reaches Earth, a considerable improvement compared to the current warning time. The launch of HENON is planned for the end of 2026. [2] [3] [4]

Contents

Background

HENON is funded through the Element 3 of the ESA's General Support Technology Programme (GSTP), [5] which supports In Orbit Demonstration of new technologies. These missions combine technology demonstration with practical applications. The mission's prime contractor is Argotec in Italy. [2]

Technologies and instruments

HENON's electric propulsion system is being developed by a UK consortium led by Mars Space. A miniature X-band space transponder and a solar array drive assembly are being developed by IMT in Italy. The spacecraft's power conditioning & distribution unit is being developed by Argotec. [2] The xenon gas gridded ion engine is similar to the one used on the BepiColombo mission to Mercury, though miniaturised for CubeSat applications. [6]

The mission will demonstrate new miniaturised scientific instruments for space weather observations including a radiation particle telescope, magnetometer, and a Faraday Cup for measuring the solar wind properties: [2]

Mission profile

HENON will be launched together with another larger spacecraft to the Sun-Earth Lagrange point 2. Then, it will use its own electric propulsion system to fly to a Distant Retrograde Orbit (DRO) of the Sun-Earth system. In this orbit, it will be passing upstream of Earth on the sunward side and get 10x nearer the Sun compared to a spacecraft in Lagrange point 1. [2]

Timeline

See also

References

  1. "HENON". ASI (in Italian). Retrieved 2025-04-11.
  2. 1 2 3 4 5 6 "ESA's first stand-alone Deep Space CubeSat signs new phase". www.esa.int. Retrieved 2025-04-03.
  3. Kulu, Erik. "HENON". Nanosats Database. Retrieved 2025-04-03.
  4. HEliospheric pioNeer for sOlar and interplanetary threats defeNce, E. M. Alessi et al.
  5. "About the General Support Technology Programme (GSTP)". www.esa.int. Retrieved 2025-04-03.
  6. 1 2 "Firing up HENON's engine". www.esa.int. Retrieved 2025-04-03.
  7. Eastwood, J. P.; Kataria, D. O.; McInnes, C. R.; Barnes, N. C.; Mulligan, P. (2015). "Sunjammer" . Weather. 70 (1): 27–30. Bibcode:2015Wthr...70...27E. doi: 10.1002/wea.2438 . ISSN   0043-1656.
  8. "A fall of CubeSats". www.esa.int. Retrieved 2025-04-03.
  9. Přech, Lubomír; Šafránková, Jana; Němeček, Zdeněk; Čermák, Ivo; Ďurovcová, Tereza; Marcucci, Maria Federica; Laurenza, Monica; Calgano, Davide (2024). Faraday cup instrument for the solar wind monitoring at 0.9 AU HENON mission (Report). Copernicus Meetings. doi: 10.5194/egusphere-egu24-10847 .