document title / titre du document TRP W ORK PLAN ... - emits - ESA

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TRP Work Plan 2005-2007 Description of Activities TEC-SB/7935/dc 12/Feb/09 TRP Reference: Title: T213-04MM Ultrasonic Tools for Planetary Surface Exploration The suitability of ultrasonic tools, e.g. for coring and drilling to limited depth (or generally sample acquisition and transportation) shall be studied and demonstrated with adequate hardware. A small initial feasibility study has been carried out by Leicester University in the frame of the AURORA programme, and has encouraged the use of ultrasonic tools for miniature sampling devices. Compared with classical mechanical corers and drills, ultrasonic equipment is very robust and simple as it does not require a high number of moving parts or a sophisticated drive mechanism. Several actuator types and mechanical amplifiers shall be studied. A major constraint is expected with the typical electric power limitations of planetary landing missions. Furthermore, the interaction of ultrasound with rock and softer materials is largely unknown. Deliverables: Demonstrator Model(s), including the ultrasonic transducer and drive electronics. Current TRL: TRL2 Target TRL: TRL3/4 Application Need/Date: TRL5 in 2008 Application/Mission: ExoMars, MSR Contract Duration: 18 months SW Clause : - Dossier0 Ref.: T-824 Consistency with Harmonisation Roadmap and Conclusions: TRP Reference: T213-06MM Title: Imaging Lidar technology Nowadays Imaging Lidars can perform measurements up to few kilometres at typical distance resolutions of a few centimetres at a rate of a few kHz. Imaging Lidars can support a number of space applications on orbiter modules, landers and planetary rovers like surface mapping, hazard avoidance and safe landing, navigation, multiple spacecraft operations (rendez-vous and docking), target properties recognition. However, since most of these systems rely on complex scanning mechanisms, they are bulky and often too heavy for future solar system exploration missions. The recent emergence of novel and advanced technologies like new 2-dimensional detector arrays (APD or CMOS arrays) and optical micro components (like MEMS and MOEMS) will bring a new trend in the development of compact, high resolution and multi-task sensor Imaging Lidars. This activity shall study the use of these novel technologies, assess the impact on the Lidar performances and develop an Imaging Lidar proof-of-concept breadboard that validates these technologies, making the Imaging Lidar a feasible instrument for space applications in the frame of AURORA. Deliverables: Imaging Lidar breadboard. Current TRL: TRL2 Target TRL: TRL3 Application Need/Date: TRL5 in 2009 Application/Mission: Aurora (ExoMars) Contract Duration: 24 months SW Clause : - Dossier0 Ref.: T-7715 Consistency with Harmonisation Roadmap and Conclusions: TRP Reference: T213-07MM Title: Down hole hammering Mechanism The objective is to develop a high-energy (0.5-2 J/impact) hammering system, that can be placed inside the drill string (20-40 mm in diameter). Power generation can utilize an electric motor, but shape memory alloys and piezo-elements (operating in an inch-worm manner) can be considered as an option. An optional passive mechanism to take impact power directly from the drill rotation (without any additional power sources and power feed-through) can also be considered. Impact frequency will be limited by the power of the actuator; however, impact energy must be kept at a level high enough to provide the desired effect. Deliverables: Breadboard of a drill- hammering device. Current TRL: TRL2 Target TRL: TRL3-4 Application Need/Date: TRL5 in 2008 Application/Mission: ExoMars, MSR Contract Duration: 18 months SW Clause : - Dossier0 Ref.: T-824 Consistency with Harmonisation Roadmap and Conclusions: Page 81 of 227
TRP Work Plan 2005-2007 Description of Activities TEC-SB/7935/dc 12/Feb/09 TRP Reference: Title: T213-08MM Biochemical analyser Bio-chemical analysis is taking an increasing importance not only for the Space Station but also for interplanetary missions, first for search for life and later for supporting manned missions. If a system can be made available for the ISS in a relatively short term, it will use commercial, wet reagents with stability span of a couple years maximum, hence not compatible with long-duration interplanetary missions without re-supply capabilities. To be interplanetary-mission compatible, both technology and consumables (i.e. the reagents) must be adapted to reduced volumes and be compatible with preservation constraints and reduced operational capabilities (the first systems will be fully automated). No system is known that may be compatible with interplanetary mission requirements. Deliverables: Feasibility assessment. Current TRL: - Target TRL: TRL2 Application Need/Date: TRL5 > 2012 Application/Mission: MSR Contract Duration: 18 months SW Clause : - Dossier0 Ref.: T-1272 Consistency with Harmonisation Roadmap and Conclusions: Page 82 of 227
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