The requirements aim to:
1) Guarantee successful disposal
ESA missions must ensure the safe disposal of space objects through atmospheric reentry or reorbiting to a safe altitude with a probability of success higher than 90%. Missions should also include interfaces that would help them be more easily removed from orbit, should self-disposal fail.
2) Improve orbital clearance
The less time an object is in orbit, the smaller the chance that it will collide with another object and create further debris. The maximum time spent in protected low-Earth orbits at end of life for new ESA missions has been reduced from 25 years to just five. There are also more stringent requirements for missions involving a constellation of satellites.
3) Avoid in-orbit collisions
Collision avoidance – manoeuvring a satellite out the way of potential collision – is now a regular part of flying missions in low-Earth orbit. With the dramatic rise of space activity and the growth in the amount of debris in orbit, the number of collision alerts received every week is also growing. Improved collision avoidance strategies – using automation, space traffic coordination, new communication protocols etc. – must be developed as the risk of collision increases.
4) Avoid internal break-ups
Satellite health monitoring must be improved, and robust passivation techniques implemented to prevent satellites breaking up from within.
5) Prevent intentional release of space debris
The intentional release of objects such as protective covers, lens caps and rocket fairings must be minimised.
6) Improve on-ground casualty risk assessment
Standardised tools and methodologies should be developed for assessing the casualty risk, on the ground, of reentering objects, as well as for verifying that a mission is designed properly for demise at end of life.
7) Guarantee dark and quiet skies
Measures must be identified and implemented to minimise the impact of space objects on optical and infrared astronomy, as well as radio astronomy, to maintain dark and quiet skies.
8) Beyond the protected regions
Other orbits, such as those used by Global Navigation Satellite System (GNSS) constellations and lunar orbits, should also be considered and protected to ensure their long-term sustainability. Adapted Zero Debris recommendations should be formulated and applied beyond low-Earth orbit and Geostationary orbit.