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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 &...
Surrey Satellite...
Surrey Satellite...
Beginning in June 2012, an MSSL-led team have performed a study of the requirements and design of a Lunar Surface Camera Package for Exploration L- CAM for the ESA Lunar Lander. However, the Lunar Lander program was terminated by the ESA Ministerial Council in November 2012. As a result, with four of the six TNs requested in the SoW completed, ESA instructed MSSL to concentrate work on the L-CAM thermal model. The following final report is therefore composed of TNs 1- 4 and the Thermal Report.
University College London
A considerable amount of supporting research and technology development has to take place on the Earth to allow humans to explore the Moon, Mars and beyond. The Concepts for Activities in the Field for Exploration (CAFE) project aims to support such aims in an international context by preparing a complete catalogue of terrestrial analogue environments that are appropriate for testing human space exploration-related scientific field activities.
The OPEN UNIVERSITY
Space capsule crew injury protection from landing forces originated from research originally conducted into fast jet ejection. There, the primary focus was on the protection of the pilot’s spine from over-compression and led to the one-dimensional Dynamic Response Index (DRI) for assessing the spinal injury potential of measured acceleration pulses.
CRANFIELD INNOVATIVE...
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.
SEA Ltd
IMPERIAL COLLEGE LONDON
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