Explore the words cloud of the C3HARME project. It provides you a very rough idea of what is the project "C3HARME" about.
The following table provides information about the project.
Coordinator |
CONSIGLIO NAZIONALE DELLE RICERCHE
Organization address contact info |
Coordinator Country | Italy [IT] |
Project website | http://c3harme.eu/ |
Total cost | 8˙033˙034 € |
EC max contribution | 8˙033˙034 € (100%) |
Programme |
1. H2020-EU.2.1.3. (INDUSTRIAL LEADERSHIP - Leadership in enabling and industrial technologies - Advanced materials) |
Code Call | H2020-NMP-2015-two-stage |
Funding Scheme | RIA |
Starting year | 2016 |
Duration (year-month-day) | from 2016-06-01 to 2020-05-31 |
Take a look of project's partnership.
There is an increasing demand for advanced materials with temperature capability in highly corrosive environments for aerospace. Rocket nozzles of solid/hybrid rocket motors must survive harsh thermochemical and mechanical environments produced by high performance solid propellants (2700-3500°C). Thermal protection systems (TPS) for space vehicles flying at Mach 7 must withstand projected service temperatures up to 2500°C associated to convective heat fluxes up to 15 MWm-2 and intense mechanical vibrations at launch and re-entry into Earth’s atmosphere. The combination of extremely hot temperatures, chemically aggressive environments and rapid heating/cooling is beyond the capabilities of current materials. Main purpose of C3HARME is to design, develop, manufacture, test and validate a new class of out-performing, reliable, cost-effective and scalable Ultra High Temperature Ceramic Matrix Composites (UHTCMCs) based on C or SiC fibres/preforms enriched with ultra-high temperature ceramics (UHTCs) capable of in-situ repairing damage induced during operation in severe aerospace environments. C3HARME will apply to two main applications: near-ZERO erosion rocket nozzles that must maintain dimensional stability during firing in combustion chambers, and near-ZERO ablation thermal protection systems enabling hypersonic space vehicles to maintain flight performance. C3HARME represents a well-balanced mix of innovative and consolidated technologies, mitigating the level of risk intrinsic in top-notch research and innovation development. C3HARME starts from TRL of 3-4 and focuses on TRL 6 thanks to a strong industrial partnership, including SMEs and large companies. To reach TRL 6, rocket nozzles and TPS tiles with realistic dimensions and shape will be fabricated, assembled into a suitable system, and validated in a relevant ambient (environment centered test). Project results could be easily extended to the energy, medical and/or nuclear environments.
Catalogue of innovations risks - month 24 | Documents, reports | 2019-08-30 14:07:31 |
Specific set of recommendations for material development in WP2 based on micro-models / DFT | Documents, reports | 2019-08-30 14:07:31 |
Summary D2.1, 2.2, 2.3, 2.4 | Documents, reports | 2019-08-30 14:07:31 |
Atomistic modelling of processes at materials interfaces | Documents, reports | 2019-08-30 14:07:31 |
Visual identity kit - 12 month | Documents, reports | 2019-08-30 14:07:29 |
Catalogue of innovations risks - month 12 | Documents, reports | 2019-08-30 14:07:29 |
Take a look to the deliverables list in detail: detailed list of C3HARME deliverables.
year | authors and title | journal | last update |
---|---|---|---|
2018 |
Yanhui Zhang, Stefano Sanvito Firstâ€principles investigation of the thermodynamic stability of M B 2 materials surfaces ( M = Ti/Zr/Hf) published pages: 4118-4127, ISSN: 0002-7820, DOI: 10.1111/jace.15547 |
Journal of the American Ceramic Society 101/9 | 2019-08-30 |
2017 |
Antonio Vinci, Luca Zoli, Elena Landi, Diletta Sciti Oxidation behaviour of a continuous carbon fibre reinforced ZrB 2 –SiC composite published pages: 129-138, ISSN: 0010-938X, DOI: 10.1016/j.corsci.2017.04.012 |
Corrosion Science 123 | 2019-08-30 |
2019 |
Antonio Vinci, Luca Zoli, Diletta Sciti, Jeremy Watts, Greg E. Hilmas, William G. Fahrenholtz Mechanical behaviour of carbon fibre reinforced TaC/SiC and ZrC/SiC composites up to 2100°C published pages: 780-787, ISSN: 0955-2219, DOI: 10.1016/j.jeurceramsoc.2018.11.017 |
Journal of the European Ceramic Society 39/4 | 2019-08-30 |
2018 |
R. Savino, S. Mungiguerra, G. D. Di Martino Testing ultra-high-temperature ceramics for thermal protection and rocket applications published pages: s9-s18, ISSN: 1743-6753, DOI: 10.1080/17436753.2018.1509175 |
Advances in Applied Ceramics 117/sup1 | 2019-08-30 |
2018 |
V. Rubio, P. Ramanujam, J. Binner Ultra-high temperature ceramic composite published pages: s56-s61, ISSN: 1743-6753, DOI: 10.1080/17436753.2018.1475140 |
Advances in Applied Ceramics 117/sup1 | 2019-08-30 |
2018 |
Mungiguerra Stefano Arc-Jet testing of ultra-high-temperature ceramic matrix composites for aerospace applications. published pages: , ISSN: , DOI: 10.5281/zenodo.2551293 |
First Workshop for Young Ceramists, Bologna, Italy, 26-27 November 2018 | 2019-08-30 |
2018 |
Marius Kütemeyer, Thomas Helmreich, Stefan Rosiwal, Dietmar Koch Influence of zirconium-based alloys on manufacturing and mechanical properties of ultra high temperature ceramic matrix composites published pages: s62-s69, ISSN: 1743-6753, DOI: 10.1080/17436753.2018.1509810 |
Advances in Applied Ceramics 117/sup1 | 2019-08-30 |
2018 |
Luca Zoli, Pietro Galizia, Laura Silvestroni, Diletta Sciti Synthesis of group IV and V metal diboride nanocrystals via borothermal reduction with sodium borohydride published pages: 2627-2637, ISSN: 0002-7820, DOI: 10.1111/jace.15401 |
Journal of the American Ceramic Society 101/6 | 2019-08-30 |
2018 |
Pietro Galizia, Simone Failla, Luca Zoli, Diletta Sciti Tough salami-inspired Cf/ZrB2 UHTCMCs produced by electrophoretic deposition published pages: 403-409, ISSN: 0955-2219, DOI: 10.1016/j.jeurceramsoc.2017.09.047 |
Journal of the European Ceramic Society 38/2 | 2019-08-30 |
2018 |
Vinci Antonio Processing and characterization of carbon fibre reinforced ZrB2/SiC/WC composites published pages: , ISSN: , DOI: 10.5281/zenodo.2551275 |
First Workshop for Young Ceramists, Bologna, Italy, 26-27 November 2018 | 2019-08-30 |
2018 |
Antonio Vinci, Luca Zoli, Diletta Sciti, Cesare Melandri, Stefano Guicciardi Understanding the mechanical properties of novel UHTCMCs through random forest and regression tree analysis published pages: 97-107, ISSN: 0264-1275, DOI: 10.1016/j.matdes.2018.02.061 |
Materials & Design 145 | 2019-08-30 |
2018 |
Antonio Vinci, Luca Zoli, Diletta Sciti Influence of SiC content on the oxidation of carbon fibre reinforced ZrB 2 /SiC composites at 1500 and 1650 °C in air published pages: 3767-3776, ISSN: 0955-2219, DOI: 10.1016/j.jeurceramsoc.2018.04.064 |
Journal of the European Ceramic Society 38/11 | 2019-08-30 |
2019 |
S. Failla, P. Galizia, L. Zoli, A. Vinci, D. Sciti Toughening effect of non-periodic fiber distribution on crack propagation energy of UHTC composites published pages: 612-618, ISSN: 0925-8388, DOI: 10.1016/j.jallcom.2018.11.043 |
Journal of Alloys and Compounds 777 | 2019-08-30 |
2018 |
Di Martino Giuseppe D.; Mungiguerra Stefano; Cecere Anselmo; Savino Raffaele; Vinci Antonio; Zoli Luca; Sciti Diletta Hybrid rockets with nozzle in ultra-high-temperature ceramic composites published pages: , ISSN: , DOI: 10.5281/zenodo.1473368 |
69th International Astronautical Congress (IAC) 1 | 2019-08-30 |
2018 |
Luca Zoli, Antonio Vinci, Pietro Galizia, Cesare Melandri, Diletta Sciti On the thermal shock resistance and mechanical properties of novel unidirectional UHTCMCs for extreme environments published pages: , ISSN: 2045-2322, DOI: 10.1038/s41598-018-27328-x |
Scientific Reports 8/1 | 2019-08-30 |
2018 |
Raffaele Savino, Luigi Criscuolo, Giuseppe Daniele Di Martino, Stefano Mungiguerra Aero-thermo-chemical characterization of ultra-high-temperature ceramics for aerospace applications published pages: 2937-2953, ISSN: 0955-2219, DOI: 10.1016/j.jeurceramsoc.2017.12.043 |
Journal of the European Ceramic Society 38/8 | 2019-08-30 |
2018 |
Laura Silvestroni, Kerstin Stricker, Diletta Sciti, Hans-Joachim Kleebe Understanding the oxidation behavior of a ZrB 2 –MoSi 2 composite at ultra-high temperatures published pages: 216-228, ISSN: 1359-6454, DOI: 10.1016/j.actamat.2018.03.042 |
Acta Materialia 151 | 2019-08-30 |
2017 |
L. Zoli, A. Vinci, L. Silvestroni, D. Sciti, M. Reece, S. Grasso Rapid spark plasma sintering to produce dense UHTCs reinforced with undamaged carbon fibres published pages: 1-7, ISSN: 0264-1275, DOI: 10.1016/j.matdes.2017.05.029 |
Materials & Design 130 | 2019-08-30 |
2018 |
Mungiguerra Stefano; Di Martino Giuseppe D.; Cecere Anselmo; Savino Raffaele; Zoli Luca; Silvestroni Laura; Sciti Diletta Characterization of carbon-fiber reinforced ultra-high-temperature ceramic matrix composites in arc-jet environment published pages: , ISSN: , DOI: 10.5281/zenodo.1473396 |
69th International Astronautical Congress (IAC) 1 | 2019-08-30 |
2017 |
L. Zoli, D. Sciti Efficacy of a ZrB2–SiC matrix in protecting C fibres from oxidation in novel UHTCMC materials published pages: 207-213, ISSN: 0264-1275, DOI: 10.1016/j.matdes.2016.09.104 |
Materials & Design 113 | 2019-08-30 |
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The information about "C3HARME" are provided by the European Opendata Portal: CORDIS opendata.
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