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Small Satellite Missions to Mars – S2M2

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).

Spain

20-P-M-HRE-02-a

Airbus
Mars Surface Platform Capabilities Study

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:

UK

20-P-M-HRE-01-b

Airbus Defence &...
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 &...

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