EGU23-3524, updated on 22 Feb 2023
https://doi.org/10.5194/egusphere-egu23-3524
EGU General Assembly 2023
© Author(s) 2023. This work is distributed under
the Creative Commons Attribution 4.0 License.

Impact of iodine injections from the suface and the small satellites using iodine propulsion system in the upper atmosphere on ozone depletion

Wuhu Feng1, John Plane2, Martyn Chipperfield3, Alfonso Saiz-Lopez4, Jean-Paul Booth5, Sarah McClory3, and Doug Kinnison6
Wuhu Feng et al.
  • 1University of Leeds, National Centre for Atmospheric Science, School of Earth and Environment, Leeds, United Kingdom of Great Britain – England, Scotland, Wales (w.feng@ncas.ac.uk)
  • 2University of Leeds, School of Chemistry, UK
  • 3University of Leeds, School of Earth and Environment, UK
  • 4Spanish National Research Council, Spain
  • 5Laboratoire de Physique des Plasma, France
  • 6NCAR, USA

Iodine has the potential to cause stratospheric ozone depletion.  However, there is still significant uncertainty concerning the magnitude of its effect, ranging from a few percent to 10% based on the literature studies. Moreover, these studies have only considered that up to  0.77±0.10 per trillion by volume (pptv) total inorganic iodine is entrained into the stratosphere from the surface emissions. Recently the first 12U CubeSat using the iodine electric propulsion was launched in November 2021 into an orbit at ~480 km. The system produces iodine ions after vaporizing solid iodine. Thus the launch of nanosatellites using iodine propulsion will inject gas-phase iodine species into the thermosphere, which upon re-entering the atmosphere could potentially cause depletion of the ozone layer and consequently impact climate. 

Here we use the 3-D Whole Atmospheric Community Climate Model (WACCM) to investigate stratospheric ozone depletion due to the launch of small satellites (e.g., CubeSats) with an iodine propulsion system and understand the potential risks caused to stratospheric ozone . We have separted the contribution to the stratospheric ozone depletion from the surface emissions of Iodine and its injection from the upper atmosphere. We have performed a number of model sensitivity runs with different additional scenarios of iodine injection at 120-140 km to explore the potential  stratospheric ozone depletion from small satellites powered in this way. For the base case scenario in the current condition (for example year 2014), a steady-state nanosatellite launch rate of 20,000/year (e.g., 8 tons of I+ injected), the perturbation to the total column ozone is negligible. However, a 10 or 100-fold increase in the mass of iodine launched into near-Earth orbit will cause significant ozone depletion. This study quantifies the extent to which the injection of iodine into the thermosphere can deplete stratospheric ozone, which will be a useful guide for limiting the population of satellites with iodine propulsions systems in low Earth orbit. The impact of iodine for the extreme large ozone depletion years (for example, 2020)  and future scenarios of the results will be also discussed.

How to cite: Feng, W., Plane, J., Chipperfield, M., Saiz-Lopez, A., Booth, J.-P., McClory, S., and Kinnison, D.: Impact of iodine injections from the suface and the small satellites using iodine propulsion system in the upper atmosphere on ozone depletion, EGU General Assembly 2023, Vienna, Austria, 24–28 Apr 2023, EGU23-3524, https://doi.org/10.5194/egusphere-egu23-3524, 2023.

Supplementary materials

Supplementary material file