Using data collected by sensors on the U.S. Department of Defense Space Test Program Satellite 6 (STP-Sat6) in geostationary orbit, scientists have found that the number of electrical discharges on a spacecraft directly correlates to the number of electrons in the surrounding environment — information that could help them better understand how to protect equipment in space.
STP-Sat6. Image credit: Northrop Grumman.
Spacecraft environment discharges (SEDs) are transient electrical breakdowns that can damage sensitive onboard electronics and communication systems.
Researchers have long known that SEDs exist, but they haven’t understood the relationship between the electrons in the space environment and SEDs.
“To do that, we needed two sensors on a single spacecraft: one that looked at the number and activity of electrons, and another that looked at the radio frequency signal,” said Dr. Amitabh Nag, a researcher at Los Alamos National Laboratory.
These SEDs are typically the result of a difference in surface charging caused by electrons accumulating on spacecraft surfaces in orbit.
Not unlike static electricity on Earth — when energy builds up as a person walks across a carpet, for example, and causes a spark when a finger touches a door handle — electrical discharges in the space environment occur when a buildup of energy on the spacecraft eventually reaches a large enough voltage that the energy is released.
STP-Sat6 has both of those sensors on board, giving the researchers a unique opportunity to simultaneously look at both radio frequency and electron activity data.
“We were able to see the rate of SEDs reported by the radio frequency sensor and compare it to the activity of electron particles within a certain voltage range,” Dr. Nag said.
“What we learned was that the peaks in SEDs correlated to peaks in electron activity.”
The authors looked at more than a year’s worth of data from the two sensors, identifying more than 270 high-rate SED periods and several hundred episodes of high electron activity.
In about three-fourths of the cases, peaks in electron activity preceded the SED events by 24 to 45 minutes.
This delay suggests that the buildup of charge from low-energy electrons plays a key role in priming the spacecraft for electrostatic discharges.
“We observed that as electron activity increases, especially in that 7.9 to 12.2 keV range, the spacecraft starts to accumulate charge,” Dr. Nag said.
“This continues until a tipping point is reached and SEDs occur.”
“That lead time opens the door for potential forecasting tools to mitigate risks.”
“Future missions could integrate real-time monitoring of low-energy electrons to predict and respond to charging events before they impact operations.”
The results appear in the journal Advances in Space Research.
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Amitabh Nag et al. 2025. Radio frequency transients correlated with electron flux measured on-board the STP-Sat6. Advances in Space Research 76 (6): 3692-3699; doi: 10.1016/j.asr.2025.07.026