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: T608-27QC Methodology for complex Micro-Propulsion Systems Space Validation The overall objective of this 12 months preparatory activity is prepare a formal validation/pre-qualification of these complex micro-systems via GSTP4 in 2005 by using a representative pre-Qualification Model (pre-QM). The idea is to build a consortium regrouping the suppliers of complex micro-systems, the final users and ESA to obtain consensus for approval of the approach to be taken for validation/pre-qualification. The results of these discussion will be reported in technical documents that will be distributed to other potential interested parties like other final users (EADS ST, Alenia, Surrey, ...) or NSAs (SNSB, ASA, ASI, CNES, DLR...) and a Round Table will be organised to obtain consensus for approval of the approach to be taken for validation of the complex micro-systems via GSTP4 in 2005 and 2006 (Proposals QCT.LM.GSTP05&06). Deliverables: Process documentation, critical analysis report, test structures description. Evaluation/reliability testing definition, results and analysis. Final report. Representative test structures, >1 sample of each critical component. Current TRL: TRL3 Target TRL: TRL3-4 Application Need/Date: TRL5 by 2009 Application/Mission: microsatellites Contract Duration: 12 months SW Clause : - Dossier0 Ref.: T-857 Consistency with Harmonisation Roadmap and Conclusions: TRP Reference: T609-22MP Title: Innovative Gas Storage in Satellites The overall objective of the proposed work is to develop and verify a Breadboard Demonstrator (BD) for a generic compression and storage system for space applications. The compressor is based on metal hydride (MH)technology with integrated thermal control system. The system is specifically targeted towards compression and storage for regenerative fuel cell systems, but adaptable to other space and terrestrial applications, both for hydrogen, oxygen and other gases where compression and storage are required. Deliverables: Compression & Storage System, Breadboard Demonstrator. Current TRL: TRL1 Target TRL: TRL3 Application Need/Date: TRL5 by 2010 Application/Mission: Application: all satellites Contract Duration: 18 months SW Clause : - Dossier0 Ref.: T-7574 Consistency with Harmonisation Roadmap and Conclusions: Page 199 of 227
TRP Work Plan 2005-2007 Description of Activities TEC-SB/7935/dc 12/Feb/09 6.19 - Structures & Pyrotechnics TRP Reference: MCS-001 Title: Ultra light Structures - Phase 1 The space community has clearly expressed an interest in lightweight inflatable structures, as a very feasible candidate for deployment and structural support of large appendages such as solar arrays, sun-shields and reflectors, needed for the next generation scientific and commercial spacecraft. Previous inflatable structures technology programmes of the European Space Agency have demonstrated the potential of complex inflatable structures (such as antennas and sunshields), and this combined with the above defined need, justifies actions foreseen to be taken in this area. The new interest for inflatable structures is fully explained by the perspectives they offer: with a lower mass and stowed volume, they may prevent the use of larger expensive launchers. Furthermore, they may offer new capabilities (large reflectors, large solar arrays, solar sails), which will open a new era in the space exploration. One can indeed imagine small satellites with large communication antennas, and increased on-board power due to large solar arrays made possible by inflatable structures. In order to further mature the inflatable structures towards a spacecraft application, a number of significant technological problems need to be solved. The final demonstration that such technologies are mastered and ready for a flight programme implementation is especially difficult. Indeed, for most of them, a validation on ground is not sufficient, or simply impossible. Therefore, steps to demonstrate feasibility of concept have to follow the logical approach of analysis, ground testing and finally a flight test demonstrator. It is the intention that this activity to: - proof maturity of the relevant technology developments; - select a flight demonstrator concept, considering not only technical requirements but also launch constraints; - complete the detailed design of the flight demonstrator; - manufacture and ground test prove the flight demonstrator (combined analysis and testing). A successful completion of this program will thus pave the way for a future European inflatable structure flight demonstration mission. Flight test would be proposed as part of the GSTP. Deliverables: Technical datapackage. Demonstrator. Current TRL: Target TRL: Application Need/Date: Application/Mission: Contract Duration: SW Clause : - Dossier0 Ref.: T-617 Consistency with Harmonisation Roadmap and Conclusions: TRP Reference: Title: Ultra light Structures - Phase 2&3 The space community has clearly expressed an interest in lightweight inflatable structures, as a very feasible candidate for deployment and structural support of large appendages such as solar arrays, sun-shields and reflectors, needed for the next generation scientific and commercial spacecraft. Previous inflatable structures technology programmes of the European Space Agency have demonstrated the potential of complex inflatable structures (such as antennas and sunshields), and this combined with the above defined need, justifies actions foreseen to be taken in this area. The new interest for inflatable structures is fully explained by the perspectives they offer: with a lower mass and stowed volume, they may prevent the use of larger expensive launchers. Furthermore, they may offer new capabilities (large reflectors, large solar arrays, solar sails), which will open a new era in the space exploration. One can indeed imagine small satellites with large communication antennas, and increased on-board power due to large solar arrays made possible by inflatable structures. In order to further mature the inflatable structures towards a spacecraft application, a number of significant technological problems need to be solved. The final demonstration that such technologies are mastered and ready for a flight programme implementation is especially difficult. Indeed, for most of them, a validation on ground is not sufficient, or simply impossible. Therefore, steps to demonstrate feasibility of concept have to follow the logical approach of analysis, ground testing and finally a flight test demonstrator. It is the intention that this activity to: Page 200 of 227
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