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This study investigated the semi-autonomous exploration of a lunar skylight cavity.
DFKI - Deutsches...
The scope of this study was to investigate the possibility of designing a wireless power transfer system from the lander to the rover, based on laser technology, to:
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Avoid the use of nuclear power systems, such as the plutonium Multi Mission Radioisotope Thermoelectric Generator (MMRTG) accommodated onboard the NASA/JPL MSL Curiosity Rover, due to the constraints imposed by the use of radioactive materials
Leonardo
The ISRU-DM mission aims to perform the first demonstration of ISRU on the Moon, via the production of water or oxygen from raw lunar material (i.e. regolith, ice etc.) At Agency-level a phase-0 level study was also performed to understand the technical and programmatic feasibility of undertaking the ISRU-DM mission via the provision of commercial services from industry.
Surrey Satellite...
The International Space Station (ISS) is slowly approaching the end of its mission. The European Space Agency (ESA) and its international partners are considering new mission targets for the future of human space exploration in the post-ISS era. Highest ranked on the list of potential targets are a return to the Moon, Near-Earth Objects or asteroids, the moons of Mars (Phobos, Deimos) and, as the ultimate target, the surface of Mars.
COMEX SA
Global plans for exploratory missions aim at extending the distances travelled by humans well beyond low Earth orbit and establishing permanent bases on the surface of Moon and Mars [1]. This will inevitably lead to increasing mission duration, radiation intensity, gravity levels and degree of confinement and isolation to which the crews will be exposed. In this extended space mission context, the astronauts should have the means to collect medical/physiological data in order to understand if their physiological conditions are in nominal levels.
CSEM SA
The objective of the project was to define, design and validate data mining algorithms that enable advanced or autonomous medical monitoring and diagnostics for astronauts, exploiting standard medical data available from health and sanitary structures.
SATE
The objective of the APPS study has been to investigate the feasibility, architectural and system design, and potential performance of a non-nuclear system whose single goal is to provide survival and servicing support to a planetary payload element, in order to ensure its operations despite the absence of sunlight for extended periods. The principle aim is to advance concepts and overall approaches to meet this goal, and to provide a framework for the future development of key technologies.
OHB System AG
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
The main goals of the DPEM project was [RD1] "to set the foundations for the development of a comprehensive suite of near surface dusty plasma environment models applicable in particular (but not only) to airless bodies of interest for future exploration missions such as asteroids, the Moon, Phobos and Deimos, etc … These models shall allow the definition of charged dust environment specifications to assess the effects of dusty plasmas on near surface or surface exploration units (spacecraft, payload, lander, astronaut) in a surface-spacecraft-dust environment system."
Finnish Meteorological...
Low energy transfers have shown that it is possible to reduce the ∆v cost (and therefore the propellant mass) for a number of transfer types. This is possible by exploiting the natural n-body dynamics characterizing the spacecraft motion within the Solar System. In particular, the concept of ballistic capture makes it possible to reduce the hyperbolic excess velocity upon moon/plant arrival, and allows the spacecraft to perform few orbits at zero cost. Low energy transfers are designed by using impulsive maneuver, and therefore they inherently use chemical propulsion (Figure 1).
DINAMICA SRL
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