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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 />

T103-28MM<br />

High Energy Fiber-based Laser and Receiver development in the 2 micron region for<br />

Title:<br />

atmospheric CO2 and other greenhouse gases measurements<br />

In the context of the third cycle of Earth Explorer Core Missions the Agency is currently investigating the technical feasibility of<br />

an active optical sensing mission to measure the concentration of atmospheric carbon dioxide (CO2). A spaceborne<br />

Differential Absorption Lidar operating at the near-infrared absorption band of CO2 around 2.05 micron constitutes one of the<br />

candidate measurement concepts. Regarding the required system performance it appears that the use of pulsed laser<br />

sources with an average power on the several Watts level offers advantages over mo<strong>du</strong>lated continuous-wave (CW) laser<br />

based concepts. In the parameter regime of modest laser pulse energy (mJ level) and kHz pulse repetition rates an all-fibre<br />

laser concept is a promising candidate. Given its intrinsically high optical efficiency, system compactness and alignment<br />

insensitivity a fibre laser offers significant assets for spaceborne implementation. On the other hand the targeted fibre laser<br />

system will have to tackle major technological challenges that come with the combination of cutting-edge pulse energies out of<br />

a fibre and highly demanding spectral requirements in particular on centre wavelength stability and spectral purity. This activity<br />

will address the development of a laser diode pumped all-fibre laser source at 2.05 micron for spaceborne CO2<br />

measurements.<br />

Deliverables:<br />

Technology demonstrators of Tx/Rx key elements.<br />

Current TRL: TRL2 Target TRL: TRL4-5 Application Need/Date: TRL5 by 2010<br />

Application/Mission: A-Scope Mission Contract Duration: 18 months<br />

SW Clause : - Dossier0 Ref.: T-419<br />

Consistency with Harmonisation<br />

Roadmap and Conclusions:<br />

Lidar Critical Solid-state Components<br />

<strong>TRP</strong> Reference: T104-13MM<br />

Title:<br />

Instrument technology for fluorescence<br />

This activity will address the development of critical technologies for the measurement of fluorescence from low Earth orbit<br />

satellites (fluorosensors). The FLEX mission aims to pro<strong>du</strong>ce global scale maps of vegetation photosynthetic activity<br />

contributing to biosphere and global carbon cycle studies. The mission is based on a three-instrument system for measuring<br />

plant fluorescence, multi-angle hyperspectral reflectance and canopy temperature. Early instrument pre-development shall be<br />

dedicated to the demonstration of the feasibility to measure the weak fluorescence signals over heterogeneous natural<br />

vegetation and to achieve high spectral resolution and spectral stability across a large field-of-view.<br />

Deliverables:<br />

Breadboard of critical instrument core unit demonstrating the achievable sensitivity of the fluorosensor.<br />

Current TRL: TRL0-1 Target TRL: TRL3 Application Need/Date: TRL5 by 2011<br />

Application/Mission:<br />

FLEX (Fluorescence Explorer) mission<br />

(selected for assessment studies for third<br />

cycle Earth Explorer Core Mission)<br />

Contract Duration:<br />

18 months<br />

SW Clause : - Dossier0 Ref.: T-419<br />

Consistency with Harmonisation<br />

Not directly linked to harmonised technology.<br />

Roadmap and Conclusions:<br />

Page 24 of 227

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