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Science in space: the CSES mission @ TIFPA

May 11, 2026

Space@TIFPA

Francesco M. Follega(1,2) for CSES-Limadou

(1) Department of Physics, University of Trento

(2) Trento Institute of Fundamental Physics and Applications (TIFPA-INFN)

S. Perciballi

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The CSES scientific mission

The CSES mission is a scientific collaboration between Italy and China. The satellites (Polar + Sun Synchronous orbit - 500 km) carries a suite of instruments for the detection of electromagnetic fields, particles and plasma in space.

Scientific goals:

  • Investigate the ionosphere and gather world-wide data;
  • Measure the particles and plasma perturbations in the ionosphere and magnetosphere: natural sources (EQs) and anthropic emitters;
  • Study solar-terrestrial interactions and solar physics: CMEs, SEPs, solar flares;
  • Study and extend low energy spectrum of cosmic rays.

Space Weather

Scientific partners

Industrial partners

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HEPD-01 on board the CSES-01 satellite

HEPD-01

CAD model

Limadou HEPD-01 integrated on CSES-01

Acceptances for

contained particles

Peak ~ 400 cm2 sr

HEPD-01 is designed to measure fluxes of charged particles: electrons (3-100 MeV) and protons (30-200 MeV) and light nuclei at low energy

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Search for particle burst with CSES-01 payloads

    • Analysis of low-energy (from 100 keV) electrons of CSES
    • Data collection, preparation, background estimation in invariant phase-space
    • Selection of exceptional events and building/clustering of particle bursts
    • Anomalous cluster analysis with ML-algorithms (DB scan)

Particle bursts search at low energies

drift

bounce

gyration

Three periodic motions of trapped particles

R. Battiston, V. Vitale / Nuclear Physics B (Proc. Suppl.) 243–244 (2013) 249–257

Time correlation EQ-PB

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Gamma Ray burst physics … The BOAT

Geant4 simulation of HEPP-L channel

Anomaly detection and stat. analysis

The GRB221009A was detected by the low energy particle detector HEPP-L on board CSES-01 with framework developed for the Particle Burst search in HEPD-02. The signal was then matched with High Energy Burst Searcher (HEBS/GECAM-C) on board SATech-01.

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Gamma Ray burst analysis with HEPD-01

First GRB catalogue for HEPD-01, in the MeV gap (0.3–50 MeV). Demonstrates HEPD-01 capability beyond its design → groundwork for HEPD-02 dedicated GRB mode. New blind search method applied.

This analysis framework allowed for the identification of Gamma Ray Burst as significative outliers in the particle rate��12 GRBs a posteriori matched with other instruments

→ fluences, T90 and Tpeak have been estimated��→ HEPD-01 GRB catalogue over the full data taking

bkg estimation (parametric approach)

bkg subtraction

(*)

“short outliers” analysis (1-2 min)

“long outliers” analysis (1-2 days)

Effective area estimation

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Research activity with HEPD-01 - Mapping the SAA

Shift of SAA centroid

Proton integral flux above threshold

Detailed particle-based mapping of the SAA above 200 MeV protons. Reference dataset for geomagnetic field evolution, space weather modeling, and space mission radiation safety. Measured northwest drift of SAA centroid and validated NASA AP9–AE9 models in poorly energy range (in this part of the 25 solar cycle).

Validation of state of the art models AP9/AE9

Synergy with COSI people for bkg estimation due to SAA passages

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Low energy cosmic ray modulation with HEPD-01

Modulation study of the protons flux in the range between 50-250 MeV (consistent with models and other detector measurement). Thanks to the HEPD-01 e/p separation power, its fluxes can be utilized to adjust modulation models for moderate to low solar activity conditions in the heliosphere

dE/dx approach to separate e/p:

  • Energy reconstruction allows for yi Ai/x
  • Geographical selection based on rigidity cut-off

Energy dependence over time (CR) allows to improve modulation models

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Time correlation and multi-payload analysis

Multi-payload and multi satellite strategy

The time correlation group in the CSES-Limadou collaboration search for space-time correlation between CSES observations and external phenomena: i.e. strong earthquakes, lightnings and VLF transmitters.

Correlation PB - transmitters (i.e NWC)

PB - lightnings (WWLLN 2019 - 2022)

Particle Wave Interaction (PB - VLF)

PB/VLF - EQ correlation

LSTM AE DNN

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The launch of the second satellite CSES-02

Jiuquan Satellite Launch Center (Inner Mongolia)

Long March 2D rocket

R.Battiston �PI of CSES-Limadou collaboration

R.Iuppa

RN-INFN of Limadou

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Multi Satellite era of the CSES mission

Operation area between lat [-65,65]

Full coverage at extreme latitudes

The new phase of the mission started with the launch of the second satellite: multi-payload and multi-satellite studies now possible

  • A new particle detectors suite for CSES-02 with improved detectors (i.e. HEPD-02) with energy range from tens of KeV to hundreds of MeV (three orders of magnitude);
  • Improved version of EFD-02 (developed by INFN) working in conjunction with EFD-01 for electromagnetic field detection;
  • Another point of observation and improved coverage and latitude span with sensitivity to GRB;

Complementary Orbit with CSES-01

  • Same Orbit Plane but shifted by 180°;
  • Return cycle: 5 days→2.5 days

EFD-02

HEPD-02

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HEPD-02 and EFD-02

4 probes to measure electric potential

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Research activity in Limadou - HEPD-02 tracker evolution

Both HEPD-01 and HEPD-02 are designed to reconstruct the particle identify and the arrival direction thanks to a silicon tracker, both with two different technologies

  • 2 planes of double sided Si microstrip detectors produced @ FBK:�- thickness 300 μm and total surface 880 cm2 �- Alternated floating and readout strips with a pitch of 182 μm�
  • This system has a spatial resolution of 50 μm;�
  • The tracker provides useful information (dE/dx) to identify particles

Limadou HEPD-01

Limadou HEPD-02

First MAPS in space, chips developed for ALICE experiment

  • 29.24 μm x 26.88 μm pixels (~ 4-5 μm single-hit resolution)
  • ALTAI chip: 512x1024 pixels -> 10 chips per stave;
  • three tracking planes for an active area of 15 x 15 cm2 each
  • Low material budget ~ 0.015 X0
  • TDAQ board developed

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Performance of the HEPD-02 tracker

Position Reconstruction and cluster size - Vertical beam

Angular Reconstruction - Vertical beam

sin𝜗

φ

Target plot

~0.7 deg offset compatible with our manual alignment

Preliminary

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Other handles HEPD-02 in particle identification with the new tracker

MSC with tracker�- discriminate low energy e-/high energy p(interacting)

Low energy e-

High energy p

Courtesy of D. Giordano

Nuclei fragments (boosted) or pion star

(isotropic)

anti-D/anti-p

from the top

vertex reconstruction

(from sec. tracks)

Incoming heavy nucleus

Courtesy of N. Puccetti and R. Nicolaidis

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New GRB capabilities with HEPD-02

New physics case fully enabled:

  • Dedicated GRB triggers for HEPD-02
  • Ev. acquisition/counting mode;
  • Time resolution ~ 5 ms

Counts / 5 ms

Counts / 5 ms

GRB trigger algorithm tested and designed in Trento @ LINAC

HEPD-02

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Preliminary gamma ray transients candidates detected in flight

GRB20250902A

GRB20250702A

Interesting candidates of gamma transients identified during commissioning (ANALYSIS STILL ONGOING/PRELIMINARY)

GRB20250804B

GRB20250830C

GRB20251016B

PRELIMINARY

PRELIMINARY

PRELIMINARY

PRELIMINARY

PRELIMINARY

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First HEPD-02 in-flight data - Improved trigger logic

TR1and

Max. observed rate ~3.2 MHz

TR1&TR2

First events collected in space by HEPD-02

After the launch of HEPD-02 on board CSES-02 the first data are coming (almost 1 year up to now). Several improvements already clear with HEPD-02 w.r.t. Its predecessor.

HEPD-01

HEPD-02

TR2&BOT

New trigger logic:�- up to 6 concurrents masks

-128 configurables orbital zones

- possibility to prescale triggers�- Avoided saturation and full-lat span

Each lon/lat with different data aq. configuration

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First HEPD-02 in-flight data

In the first data we have already evidence of light nuclei signal (He) and of heavier nuclei recorded by the HEPD-02 during the first few months after commissioning

Helium signal in a few months of HEPD-02 data

Signal from heavier nuclei as in Carbon and Oxygen

Satellite always operational over the full latitude span

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Space Weather events during HEPD-02 data taking

Article in preparation for sub…

The GLE Of November 11, 2025

The January 2026 geomagnetic storm

Under submission on SW AGU

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New technologies studied/applied in the context of the CSES mission

Trained on HEPD-02 Simulation

Simulation @CNAF

+

Impact positions

and

track residuals

Calo

plane

Tracker data

Layer 1

Layer 3

FCNN

Input from

Tracker and calorimeter

fcl

fcl

PID

Ekin

Cluster Size + angles�

Input from Tracking algo

Trigger

bar

Lyso bar

CNN

Input from

Tracker images

Layer 2

Layer 3

Tracker data

HEPD-02 deep learning reconstruction chain

Deep learning event reconstruction:�

  • Limadou HEPD-01 and HEPD-02 are among the few space experiments with a full DL evReco chain�
  • Currently experimenting with state of the art models as Transformers (self-attentnion used in LLM, i.e. chatGPT or Claude AI)

R&D silici spazio

Space-Ready Silicon Tracking Technologies

  • Develop and mature MAPS/FD-MAPS and LGAD technologies for future high-energy cosmic-ray spectrometers in space.

- Moving from 180 nm to 65 nm technology enables a more compact chip design.

- Reduced power consumption, a key advantage for space missions with strict power and thermal constraints.

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Interesting times ahead…

The addition of the second satellite to the CSES mission enriches the data coverage of the mission and extends the lifetime and scientific reach of the mission and of the CSES-Limadou collaboration:

  • Improved satellite platform and possibility to acquire data on the full latitude span (higher duty cycle).�
  • Improved instruments on CSES-02:

- HEPD-02: improved tracking and PID capabilities, improved trigger logic (intelligent trigger and GRB algorithm)

- EFD-02: payload designed by INFN with several improvements which improves EFD-01

Already interesting results in less then one year:��- Two SW events detected;�- Preliminary heavy nuclei and GRBs identified;�- improved overall performance;

GRB20251016B

PRELIMINARY

New possibility of multi-payload and multi-satellite observations�Stay tuned…..

Under submission on SW AGU

Preliminary data

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Research activity in Limadou - Quest for antimatter with HEPD-02

Example of annihilation process in TR2.

pion star

(isotropic)

anti-D/anti-p

from the top

HEPD-02 may be sensitive to anti-deuterons (anti-protons) in the range between 10 MeV/n and 30 MeV/n.

vertex reconstruction

(from sec. tracks)

Antideuteron spectra from J. Heisig et al, DarkRayNet: Emulation of cosmic-ray antideuteron fluxes from dark matter �Sensitivieties of AMS-02 from F. Giovacchini et al. Cosmic Rays Antideuteron Sensitivity for AMS-02 experiment�Sensitivieties of GAPS from The GAPS experiment: low-energy antinuclei measurements for dark matter searches

preliminary

preliminary

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Research activity in Limadou - Helium and electrons with HEPD-01

Helium with HEPD-01

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