Explore the words cloud of the Rheform project. It provides you a very rough idea of what is the project "Rheform" about.
The following table provides information about the project.
Coordinator |
DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
Organization address contact info |
Coordinator Country | Germany [DE] |
Project website | http://rheform-h2020.eu/ |
Total cost | 3˙787˙553 € |
EC max contribution | 3˙787˙553 € (100%) |
Programme |
1. H2020-EU.2.1.6.1. (Enabling European competitiveness, non-dependence and innovation of the European space sector) |
Code Call | H2020-COMPET-2014 |
Funding Scheme | RIA |
Starting year | 2015 |
Duration (year-month-day) | from 2015-01-01 to 2017-12-31 |
Take a look of project's partnership.
# | ||||
---|---|---|---|---|
1 | DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV | DE (KOELN) | coordinator | 710˙505.00 |
2 | ECAPS AB | SE (SOLNA) | participant | 933˙750.00 |
3 | FOTEC FORSCHUNGS- UND TECHNOLOGIETRANSFER GMBH | AT (WIENER NEUSTADT) | participant | 572˙250.00 |
4 | AIRBUS DEFENCE & SPACE GMBH | DE (TAUFKIRCHEN) | participant | 538˙750.00 |
5 | TOTALFORSVARETS FORSKNINGSINSTITUT | SE (STOCKHOLM) | participant | 455˙103.00 |
6 | CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE CNRS | FR (PARIS) | participant | 390˙945.00 |
7 | LITHOZ GMBH | AT (WIEN) | participant | 186˙250.00 |
8 | AIRBUS DS GMBH | DE (TAUFKIRCHEN) | participant | 0.00 |
'The project deals with the replacement of hydrazine within space propulsion systems. It improves significantly the ADN-based propellants currently existing and enables the replacement of hydrazine within the whole operational area of currently used hydrazine propulsion systems. The objectives of the project are: 1.) Replacing hydrazine by adapting the propellant to currently existing materials available in Europe 2.) Development of a cold-start capable ignition system to replace hydrazine in the whole operational area 3.) Verification of the technology within battleship unit(s) to reach a Technology Readiness Level of 5 4.) Adapted numerical models to describe the processes within such propulsion systems. To reach these objectives, the following development will be done within the project A) Propellant development in order to obtain maximal temperatures within the combustion chamber that can be withstand with currently available materials in Europe. Additionally, the propellant will have increased specific impulses in relation to hydrazine. B) Development of catalytic ignition systems to withstand the thermal and mechanical shocks while having cold-start capability C) Design and testing of the corresponding battleship units within the project to verify the achievement of the project experimentally (reach TRL of 5) D) Generating validation results for future purposes to adapt the technology to future purposes. Therefore, the relation to the work programme 'Alternative to hydrazine in Europe' is achieved by a replacement of the currently hydrazine based propulsion system with a green propellant system with higher specific impulse. '
R9.4 | Documents, reports | 2019-05-06 12:56:42 |
Take a look to the deliverables list in detail: detailed list of Rheform deliverables.
year | authors and title | journal | last update |
---|---|---|---|
2017 |
C. Maleix et al. Development of catalytic materials for decomposition of ADN-based monopropellants (EUCASS), Milano, 2017 published pages: , ISSN: , DOI: 10.13009/eucass2017-479 |
7th European Conference for Aeronautics and Space Sciences | 2019-05-29 |
2017 |
M. Negri et al. Technology development for ADN-based green monopropellant thrusters - an overview of the Rheform project published pages: , ISSN: , DOI: 10.13009/eucass2017-319 |
7th European Conference for Aeronautics and Space Sciences (EUCASS) | 2019-05-29 |
2017 |
Robert-Jan Koopmans et al. Performance Comparison between Extruded and Printed Ceramic Monoliths for Catalysts published pages: , ISSN: , DOI: 10.13009/eucass2017-349 |
7th European Conference for Aeronautics and Space Sciences | 2019-05-29 |
2017 |
R.-J. Koopmans et al. Catalyst Development and Testing for ADN-Fuel Blends published pages: , ISSN: , DOI: |
68th International Astonautical Congress | 2019-05-29 |
2017 |
C. Hendrich et al. Ignition of ADN-based Monopropellants - Results of the European Project Rheform published pages: , ISSN: , DOI: |
68th International Astonautical Congress | 2019-05-29 |
2017 |
Ulrich Gotzig Challenges and Economic Benefits of Green Propellants for Satellite Propulsion published pages: , ISSN: , DOI: 10.13009/eucass2017-639 |
7th European Conference for Aeronautics and Space Sciences (EUCASS) | 2019-05-29 |
2018 |
Michele Negri, Marius Wilhelm, Christian Hendrich, Niklas Wingborg, Linus Gediminas, Leif Adelöw, Corentin Maleix, Pierre Chabernaud, Rachid Brahmi, Romain Beauchet, Yann Batonneau, Charles Kappenstein, Robert-Jan Koopmans, Sebastian Schuh, Tobias Bartok, Carsten Scharlemann, Ulrich Gotzig, Martin Schwentenwein New technologies for ammonium dinitramide based monopropellant thrusters – The project RHEFORM published pages: 105-117, ISSN: 0094-5765, DOI: 10.1016/j.actaastro.2017.11.016 |
Acta Astronautica 143 | 2019-05-24 |
2016 |
M. Negri, C. Hendrich, M.Wilhelm, D. Freudenmann, H. K. Ciezki
L. Gediminas, L. Adelöw Thermal Ignition of ADN-based Propellants published pages: , ISSN: , DOI: |
Space Propulsion Conference 2016, Rome 02-06 May 2016 | 2019-05-24 |
2015 |
Michele Negri Replacement of Hydrazine: Overview and First Results of the H2020 Project Rheform published pages: , ISSN: , DOI: |
6TH European Conference for Aeronautics and Space Sciences (EUCASS) 29 June - 3 July 2015 | 2019-05-24 |
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The information about "RHEFORM" are provided by the European Opendata Portal: CORDIS opendata.