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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
Airbus Defence &...
In traditional data processing and control architectures for space systems, one or a few centralised computing nodes are used.
All sensors, actuators, and other data sources and data sinks are connected to these nodes in a star– or multi-star topology. Actuators and associated sensors (e.g. heaters and associated temperature sensors) are usually kept separate, with individual harnesses connecting them to the central nodes.
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