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Development of UHTCMCs via water based ZrB2 powder slurry infiltration and polymer infiltration and pyrolysis

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Visual identity kit - 12 month

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Efficacy of a ZrB2–SiC matrix in protecting C fibres from oxidation in novel UHTCMC materials

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Catalogue of innovations risks - month 24

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Catalogue of innovations risks - month 12

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Visual identity kit - 48 month

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

PROCESS FOR OBTAINING COMPOSITE, ULTRA-REFRACTORY, FIBRE-REINFORCED CERAMIC MATERIALS

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Merging toughness and oxidation resistance in a light ZrB2 composite

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Selection, processing, properties and applications of ultra-high temperature ceramic matrix composites, UHTCMCs – a re...

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

A simple route to fabricate strong boride hierarchical composites for use at ultra-high temperature

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Is spark plasma sintering suitable for the densification of continuous carbon fibre - UHTCMCs?

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Off-axis damage tolerance of fiber-reinforced composites for aerospace systems

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Pushing the limits of atomistic simulations towards ultra-high temperature: A machine-learning force field for ZrB2

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Ti3SiC2-Cf composites by spark plasma sintering: Processing, microstructure and thermo-mechanical properties

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Ablation behaviour of ultra-high temperature ceramic matrix composites: Role of MeSi2 addition

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Impact of residual stress on thermal damage accumulation, and Young's modulus of fiber-reinforced ultra-high temperature...

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Influence of fibre content on the strength of carbon fibre reinforced HfC/SiC composites up to 2100 °C

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Oxidation behaviour of a continuous carbon fibre reinforced ZrB 2 –SiC composite

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Interface engineering of graphene nanosheet reinforced ZrB 2 composites by tuning surface contacts

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Processing and characterization of carbon fibre reinforced ZrB2/SiC/WC composites

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Ultra-High-Temperature Ceramic Matrix Composites in Hybrid Rocket Propulsion Environment

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Toughening effect of non-periodic fiber distribution on crack propagation energy of UHTC composites

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Testing ultra-high-temperature ceramics for thermal protection and rocket applications

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Influence of SiC content on the oxidation of carbon fibre reinforced ZrB 2 /SiC composites at 1500 and 1650 °C in air

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Influence of zirconium-based alloys on manufacturing and mechanical properties of ultra high temperature ceramic matrix ...

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Mechanical behaviour of carbon fibre reinforced TaC/SiC and ZrC/SiC composites up to 2100°C

Project: C3HARME

Updated at: 29-04-2024

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Project acronym C3HARME

Resources

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Development of UHTCMCs via water based ZrB2 powder slurry infiltration and polymer infiltration and pyrolysis

Visual identity kit - 12 month

Efficacy of a ZrB2–SiC matrix in protecting C fibres from oxidation in novel UHTCMC materials

Catalogue of innovations risks - month 24

Catalogue of innovations risks - month 12

Visual identity kit - 48 month

PROCESS FOR OBTAINING COMPOSITE, ULTRA-REFRACTORY, FIBRE-REINFORCED CERAMIC MATERIALS

Merging toughness and oxidation resistance in a light ZrB2 composite

Selection, processing, properties and applications of ultra-high temperature ceramic matrix composites, UHTCMCs – a re...

A simple route to fabricate strong boride hierarchical composites for use at ultra-high temperature

Is spark plasma sintering suitable for the densification of continuous carbon fibre - UHTCMCs?

Off-axis damage tolerance of fiber-reinforced composites for aerospace systems

Pushing the limits of atomistic simulations towards ultra-high temperature: A machine-learning force field for ZrB2

Ti3SiC2-Cf composites by spark plasma sintering: Processing, microstructure and thermo-mechanical properties

Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment

Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC

Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles

Ablation behaviour of ultra-high temperature ceramic matrix composites: Role of MeSi2 addition

Impact of residual stress on thermal damage accumulation, and Young's modulus of fiber-reinforced ultra-high temperature...

Influence of fibre content on the strength of carbon fibre reinforced HfC/SiC composites up to 2100 °C

Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites

Oxidation behaviour of a continuous carbon fibre reinforced ZrB 2 –SiC composite

Interface engineering of graphene nanosheet reinforced ZrB 2 composites by tuning surface contacts

Processing and characterization of carbon fibre reinforced ZrB2/SiC/WC composites

Ultra-High-Temperature Ceramic Matrix Composites in Hybrid Rocket Propulsion Environment

Toughening effect of non-periodic fiber distribution on crack propagation energy of UHTC composites

Testing ultra-high-temperature ceramics for thermal protection and rocket applications

Influence of SiC content on the oxidation of carbon fibre reinforced ZrB 2 /SiC composites at 1500 and 1650 °C in air

Influence of zirconium-based alloys on manufacturing and mechanical properties of ultra high temperature ceramic matrix ...

Mechanical behaviour of carbon fibre reinforced TaC/SiC and ZrC/SiC composites up to 2100°C