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

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<strong>TRP</strong> Work Plan 2005-2007<br />

Description of Activities<br />

TEC-SB/7935/dc<br />

12/Feb/09<br />

<strong>TRP</strong> Reference:<br />

Title:<br />

T213-04MM<br />

Ultrasonic Tools for Planetary Surface Exploration<br />

The suitability of ultrasonic tools, e.g. for coring and drilling to limited depth (or generally sample acquisition and<br />

transportation) shall be studied and demonstrated with adequate hardware. A small initial feasibility study has been carried out<br />

by Leicester University in the frame of the AURORA programme, and has encouraged the use of ultrasonic tools for miniature<br />

sampling devices. Compared with classical mechanical corers and drills, ultrasonic equipment is very robust and simple as it<br />

does not require a high number of moving parts or a sophisticated drive mechanism. Several actuator types and mechanical<br />

amplifiers shall be studied. A major constraint is expected with the typical electric power limitations of planetary landing<br />

missions. Furthermore, the interaction of ultrasound with rock and softer materials is largely unknown.<br />

Deliverables:<br />

Demonstrator Model(s), including the ultrasonic trans<strong>du</strong>cer and drive electronics.<br />

Current TRL: TRL2 Target TRL: TRL3/4 Application Need/Date: TRL5 in 2008<br />

Application/Mission: ExoMars, MSR Contract Duration: 18 months<br />

SW Clause : - Dossier0 Ref.: T-824<br />

Consistency with Harmonisation<br />

Roadmap and Conclusions:<br />

<strong>TRP</strong> Reference: T213-06MM<br />

Title:<br />

Imaging Lidar technology<br />

Nowadays Imaging Lidars can perform measurements up to few kilometres at typical distance resolutions of a few centimetres<br />

at a rate of a few kHz. Imaging Lidars can support a number of space applications on orbiter mo<strong>du</strong>les, landers and planetary<br />

rovers like surface mapping, hazard avoidance and safe landing, navigation, multiple spacecraft operations (rendez-vous and<br />

docking), target properties recognition. However, since most of these systems rely on complex scanning mechanisms, they<br />

are bulky and often too heavy for future solar system exploration missions. The recent emergence of novel and advanced<br />

technologies like new 2-dimensional detector arrays (APD or CMOS arrays) and optical micro components (like MEMS and<br />

MOEMS) will bring a new trend in the development of compact, high resolution and multi-task sensor Imaging Lidars. This<br />

activity shall study the use of these novel technologies, assess the impact on the Lidar performances and develop an Imaging<br />

Lidar proof-of-concept breadboard that validates these technologies, making the Imaging Lidar a feasible instrument for space<br />

applications in the frame of AURORA.<br />

Deliverables:<br />

Imaging Lidar breadboard.<br />

Current TRL: TRL2 Target TRL: TRL3 Application Need/Date: TRL5 in 2009<br />

Application/Mission: Aurora (ExoMars) Contract Duration: 24 months<br />

SW Clause : - Dossier0 Ref.: T-7715<br />

Consistency with Harmonisation<br />

Roadmap and Conclusions:<br />

<strong>TRP</strong> Reference: T213-07MM<br />

Title:<br />

Down hole hammering Mechanism<br />

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<br />

mm in diameter). Power generation can utilize an electric motor, but shape memory alloys and piezo-elements (operating in<br />

an inch-worm manner) can be considered as an option. An optional passive mechanism to take impact power directly from the<br />

drill rotation (without any additional power sources and power feed-through) can also be considered. Impact frequency will be<br />

limited by the power of the actuator; however, impact energy must be kept at a level high enough to provide the desired effect.<br />

Deliverables:<br />

Breadboard of a drill- hammering device.<br />

Current TRL: TRL2 Target TRL: TRL3-4 Application Need/Date: TRL5 in 2008<br />

Application/Mission: ExoMars, MSR Contract Duration: 18 months<br />

SW Clause : - Dossier0 Ref.: T-824<br />

Consistency with Harmonisation<br />

Roadmap and Conclusions:<br />

Page 81 of 227

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