End of Life operations for disposal of mega‐constellations
Programme Reference
15/052
Status
Closed
Country
Germany
Start Date
2017
End Date
2018
Programme: Discovery Prime Contractor: Airbus Defence & Space
Description
The objective of this activity was to understand the operational complexity of large mega-constellation systems, and the potential needs to operate these, including the complexity of collision avoidance manoeuvres (CAMs). This objective was achieved by:Assessing different end-of-life strategies for mega-constellations of the size and complexity as foreseen for the future telecommunications applications.Analysing the implications on space and ground segment design to support execution of end-of-life activities for each of the strategies identified (from the previous bullet), comparing the different ground and spacecraft conceptual architectures.Analysing the execution of both debris and inter-satellite CAMs during LEOP, orbit raising, routine phases and orbit lowering for mega-constellations.Deriving system and operational requirements on mega-constellations for end-of-life activities and space debris mitigation.Establishing a baseline scenario for an operational concept to handle space debris mitigation for mega-constellations.
• Application domain: Space Safety
•
Technology Domain:
11 - Space Debris
11 - Space Debris
•
Competence Domain:
10 - Astrodynamics / Space Debris / Space Environment
10 - Astrodynamics / Space Debris / Space Environment
• Initial TRL: TRL N/A
• Target TRL: TRL N/A
• Achieved TRL: TRL N/A
•Public Document: