“The challenge lies in the inability to accurately predict its trajectory over extended periods. Potential collision risks (close approaches to a dangerous distance) become known roughly two days before the event, at which point protocols for calculating an avoidance maneuver are initiated,” explained Alexander Ledkov, an associate professor at Samara University's Department of Theoretical Mechanics.
“We identified 289 objects over 1 kg in mass that could theoretically pose a threat to the ISS. For each, we simulated a maneuver where the spacecraft detached, intercepted the debris's orbital plane, approached within 10 meters, and redirected it using ion streams,” said the researcher.
“In the most favorable scenario, where both the debris (e.g., a rocket stage weighing about 1,400 kg) and the ISS move in the same orbital plane, our method could save 90% of the fuel. A traditional ISS orbit correction requires around 2,000 kg of fuel, whereas our spacecraft would use just over 200 kg,” added Vladimir Aslanov, a professor at the Department of Theoretical Mechanics.