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Mars Hopper Concept Technologies

Proof of Mars Hopper Concept Technologies was an eight-month study funded by ESA’s General Studies Programme from ECSAT in Harwell. The study has focussed on increasing the TRL of key technologies required for the Mars Hopper concept, which were:
- In Situ Resource Utilisation (ISRU) subsystem to collect and store CO2 from the atmosphere and deliver it to the propulsion system. Locally generated propellant doe snot require transportation to Mars providing a huge mass saving

UK

2013-2

Airbus Defence &...
Atom Interferometry Test of the Weak Equivalence Principle in Space parallel studies

The purpose of the “Atom Interferometry Test of the Weak Equivalence Principle in Space” study was to conceive and specify an instrument for an atom interferometry test of the Weak Equivalence Principle (Quantum WEP test, QWEP), focusing on the International Space Station (ISS) as space platform.

Italy

2012-16

Thales Alenia Space
Universal parts Fabricator-Replicator for Space Applications
Italy

2010-19

Thales Alenia Space
Universal parts Fabricator-Replicator for Space Applications
Italy

2010-45

Thales Alenia Space

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