SMARTIE (Smart Resource Management based on Internet of Things to support Off-Earth Manufacturing of Lunar Infrastructures) is an ESA study to assess the requirements, architecture, hardware and software needs and costs for implementation of an Internet of Manufacturing Things (IoMT) for a lunar human base and associated infrastructure. 

One of the issues facing the development of manned, long duration space missions is how to manage liquids/gases for life support. Gases such as O2, CO2, CH4 etc are inputs and by-products of life support systems, for non-regenerative (open-loop) systems. Stores should be enough to sustain any short duration crew visit and until regenerating (closed loop) systems can be installed.

New L2 missions like Euclid and Plato will require high data rate reception in K-Band downlink (26 GHz). A new X/K-Band coaxial feed system was developed in a previous TRP activity and it will be deployed in the next years in DSA2 (Cebreros, Spain) and DSA3 (Malargue, Argentina). This feed system architecture will be considered the starting point for the re-design of a new feed system that will allow simultaneous uplink (22 GHz) and downlink (26 GHz).It is intended to trade-off at least two alternative feed system architectures and to perform the detailed design of the selected one.

The objective of this study was to help define how to maintain and further develop European access to the surface of Mars, the major destination for European exploration, following the most recent approved and developed (or currently in development) missions (ExoMars 2016, ExoMars RSP).

The activity 'Small Satellite Missions to Mars (S2M2)' is an early-phase architecture study of a potential low-cost mission to Mars as further step in the Mars exploration roadmap developed by ESA.

A potential implementation from industry’s point of view was assessed, applying the strict design-to-cost philosophy by fostering strong reuse of an available OHB platform. Trade-offs were performed for assessing a low-cost mission profile targeting the programmatic constraints that were input to this study.

The aim of this study was to investigate potential small mission architectures that would further ESA's exploration objectives at Mars post-Mars Sample Return (in the 2030s) or potentially in parallel with MSR (if sufficiently low cost).

As on Earth, space debris should not only be seen as a threat. Instead, the value of waste as a recycled good should be understood. On Earth, this potential is already fully recognised. The German recycling industry alone generates more revenue than the entire European space industry. Nevertheless, this treasure was never lifted in space.

The Mars Surface Platform Capabilities Study aimed to provide ESA with an assessment of the state of the art in Mars lander technologies using ESA/European technologies with flight heritage. Airbus’ Mars lander experience is taken from the Beagle 2 probe launched in 2003 on board Mars Express.

The objectives of the study were to: