document title / titre du document TRP W ORK PLAN ... - emits - ESA
document title / titre du document TRP W ORK PLAN ... - emits - ESA
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: 03/W35<br />
Title:<br />
Martian <strong>du</strong>st simulation facility for solar cells<br />
The differences between the Mars environment and the orbital environment in which the solar cells are most commonly used<br />
require dedicated facilities to test both the solar cell and the photovoltaic assembly Coupons.<br />
The critical differences between the two environments having strong impacts in the solar cell and photovoltaic assembly<br />
testing are:<br />
- Solar intensity and spectrum modified by <strong>du</strong>st<br />
- Low temperature operation<br />
- Dust deposition on the solar array surface<br />
The Martian <strong>du</strong>st does not remain suspended in the atmosphere, but deposits out of the atmosphere onto any horizontal<br />
surfaces with a <strong>du</strong>st coverage rate of 0.3 % power loss per day. This is potentially the major lifetime limiting factor for a solar<br />
power system on any Mars mission longer than 100 sols.<br />
For this particular reason it is very important to upgrade and to modify existing test facilities that could allow the<br />
characterization and the qualification of the photovoltaic components under representative Martian <strong>du</strong>st conditions so as to<br />
timely match the needs of future Aurora missions on the surface of Mars.<br />
To achieve the above mentioned technical objective, the following activity is proposed:<br />
- Development of a Martian <strong>du</strong>st simulating facility for solar cells and coupons by modifying an already existing Wind Tunnel<br />
facility.<br />
This activity will be mainly devoted to the realization of an environmental test chamber aimed at blowing representative Mars<br />
<strong>du</strong>st over the samples in order to perform specified <strong>du</strong>st adhesion experiments.<br />
The activity will be based on a Mars Dust and Environment Specification to be provided by <strong>ESA</strong>. Special emphasis will be<br />
more particularly placed on the definition of the detailed composition of representative Martian <strong>du</strong>st particulates and of the<br />
environmental conditions to be repro<strong>du</strong>ced under testing. This test specification will be elaborated in the currently running<br />
Aurora technology activity, <strong>title</strong>d Solar Array design and technology development for Mars exploration missions.<br />
Deliverables:<br />
Development of Martian <strong>du</strong>st simulating facility for solar cells/coupons by modifying an already existing Wind Tunnel facility<br />
(Mars <strong>du</strong>st particulate/environment study and consequent realization of an environmental test chamber).<br />
Current TRL: TRL1 Target TRL: TRL4-5 Application Need/Date: TRL5 in 2009<br />
Application/Mission: Mars Exploration Contract Duration: 18 months<br />
SW Clause : - Dossier0 Ref.: T-7720<br />
Consistency with Harmonisation<br />
Roadmap and Conclusions:<br />
Solar Generators & Solar Cells<br />
<strong>TRP</strong> Reference: 04/G15<br />
Title:<br />
Precision landing GNC test facility<br />
To mitigate technical, sche<strong>du</strong>le and cost associated with enabling GNC technologies of future planetary missions requiring<br />
safe precision landing, they have to be tested as much as possible on ground in a precision landing GNC test facility. The<br />
main objective of the activity is to develop a precision landing GNC test facility that will emulate real lander dynamics and test<br />
safe precision landing navigation, guidance and control technologies to the performance level required by future planetary<br />
landing vehicles. Starting from the outputs of the on-going activity on "Verification Strategy for Smart Lander", the activity will<br />
involve: (1) analysis and trade-offs of precision landing GNC test facility configurations, inc. test facility requirements definition;<br />
(2) mechanical and electrical detailed design of the selected baseline test facility configuration; (3) manufacturing, assembly,<br />
acceptance tests and test campaign definition, and (4) integration of smart lander technologies from on-going <strong>TRP</strong> activities<br />
and test campaign results analysis.<br />
Deliverables:<br />
Precision Landing GNC Test Facility; Documentations (technical data package, summary report and abstract), including<br />
precision landing test facility configuration trade-offs/analysis, detailed design, test results, GNC SW demonstrator, test<br />
plan/results.<br />
Current TRL: TRL2 Target TRL: TRL4-5 Application Need/Date: TR5 in 2008<br />
Application/Mission: ExoMars, MSR Contract Duration: 24 months<br />
SW Clause : Operational SW Dossier0 Ref.: T-8071<br />
Consistency with Harmonisation<br />
Roadmap and Conclusions:<br />
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