UK scientists to tackle increasing problems caused by space junk

Scientists at the UK’s Defence Science and Technology Laboratory (Dstl) are leading an innovative experiment to tackle the growing problem of space junk.

Hundreds of thousands of manmade objects orbit the Earth, but fewer than 5,000 are operational satellites. The most congested area sits within 2000km of the Earth’s surface, known as low Earth orbit (LEO), where collisions can cause further debris. If this problem is not addressed, space junk threatens to make space exploration and satellite launches impossible. It also poses a hazard to existing satellites, which make an important contribution to the UK’s military capability.

To tackle this problem, the Inter-Agency Space Debris Coordination Committee (IADC) has proposed that all LEO satellites should be de-orbited within 25 years.

However, the traditional de-orbiting rocket method is expensive. As part of a large collaboration with industry, government and academia, Dstl space scientists are leading in exploring alternative methods.

The Daedalus experiment – part of the Space Situational Awareness Project in Dstl’s Space Programme – is exploring the effect on satellites of so-called Icarus ‘de-orbit sails’, made of 25 micrometre-thick aluminium-coated Kapton, a high heat-resistant polyimide film. When deployed, the sail increases drag, causing a controlled descent into the Earth’s atmosphere where the satellite will burn up.

Sean Murphy, a principal scientist in Dstl’s Space Programme, said: “It’s vitally important that we remove satellites that have reached end of life so they don’t remain in orbit as pieces of space junk.”

The first Daedalus trial has just started. A Canadian satellite, known as CanX-7, deployed its de-orbiting sail in early May 2017 and is expected to burn up in the Earth’s atmosphere in around two years’ time. Two other satellites have been fitted with Icarus de-orbit sails created by Cranfield University and are expected to start their descents later this year.

The experiment results will help to characterise changes in the brightness of the satellite caused by the sail deployment, quantify the drag increase that is due to the de-orbit sail, and critically compare different orbital dynamics models.