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:<br />
Title:<br />
T601-36MM<br />
Unlimited resetable, no-shock Hold-Down and Release Mechanism (HDRM)<br />
A worst case environmental test of the double stage Harmonic drive gear box must be performed to ensure that the gearbox<br />
behaves as expected within the specified temperature range [Operational -130 degC to + 116 degC, Survival -180 degC to<br />
+116 degC]<br />
Deliverables:<br />
HDRM breadboard model with associated datapackage <strong>document</strong>ation.<br />
Current TRL: TRL1 Target TRL: TRL3-4 Application Need/Date: TRL5 >2009<br />
Low mass appendages, where access is<br />
Application/Mission: critical (e.g. optical payload mechanisms, Contract Duration: 18 months<br />
small reflectors, covers)<br />
SW Clause : - Dossier0 Ref.: T-7847<br />
Consistency with Harmonisation<br />
Roadmap and Conclusions:<br />
Hold-down and Separation Systems<br />
<strong>TRP</strong> Reference: T601-47MX / MMM-960<br />
Title:<br />
Tribology Application Programme<br />
Within the identified funding limitations, the R&D activities proposed will address in detail all subjects from tribological design,<br />
analysis, to development and lifetime test demonstration of advanced tribological components and lubrication solutions. Tool<br />
developments to facilitate the design and analysis of bearings and its components (cages) under specialised conditions as<br />
experienced on Earth Observation payloads are included. Furthermore, moving electrical contacts, sizing for stiction and<br />
dynamic friction, and tribological solutions for miniaturised mechanisms components and development of special tribological<br />
coatings to re<strong>du</strong>ce payload and S/C cost for integration will be investigated.<br />
Deliverables:<br />
Tribological assessments, feasibility demonstrations of lubricants wrt. wear and lifetime performance, Software breadboard<br />
verifications of advanced lubricant solutions on key mechanisms components.<br />
Current TRL: - Target TRL: TRL3-4 Application Need/Date: N/A<br />
Application/Mission: all space missions Contract Duration: 60 months<br />
SW Clause : Operational SW Dossier0 Ref.: T-7846<br />
Consistency with Harmonisation<br />
Roadmap and Conclusions:<br />
Not directly linked to harmonised technology.<br />
<strong>TRP</strong> Reference: T608-31MM<br />
Title:<br />
Fully Variable Bearing Active Preload System<br />
The proposed activity aims at the development of a device that allows to actively control in-orbit the preload of ball bearings<br />
for applications requiring an extremely long life (e.g. Wheels, Pointing & Scanning mechanisms). The basic concept of<br />
bi-stable (one shot) operation, i.e. switching between high and low preload already proven in terms of concept, shall be<br />
extended to in-orbit full adjustment capability. Upon external command, it shall be possible to select a high preload and to vary<br />
a low preload setting within an appropriate range. Using a suitable target wheel as test bed, an engineering model of the<br />
preload adjustment device shall be designed, manufactured, integrated and tested in representative environment.<br />
Deliverables:<br />
Engineering Model (accompanied by Technical Data Package and further <strong>document</strong>ation).<br />
Current TRL: TRL3 Target TRL: TRL5-6 Application Need/Date: TRL5-6 in 2008<br />
Wheels, Pointing mechanisms,<br />
Application/Mission: Contract Duration: 18 months<br />
Scanning mechanisms<br />
SW Clause : - Dossier0 Ref.: T-7848<br />
Consistency with Harmonisation<br />
Roadmap and Conclusions:<br />
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