Hola,
¿eres nuevo aquí?

Regístrate gratis y conecta tu empresa con financiación pública, partners y proyectos.

Tengo cuenta

Regístrate

Ver video

GREENLAM

Financiado

Lightweight, Cost-effective Composite and Green Bipropellant System for Space Tr...

Lightweight, Cost-effective Composite and Green Bipropellant System for Space Transportation Applications "Engineering novel materials and their design optimization using simulation-based tools enable the development of lightweight and sturdy thrusters. In Europe, the development of high-temperature-resistant structural materials for... ver más

31/12/2025

TU Delft

254K€

Presupuesto del proyecto: 254K€

Líder del proyecto

TECHNISCHE UNIVERSITEIT DELFT No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Ver 2 Participantes

Financiación concedida El organismo HORIZON EUROPE notifico la concesión del proyecto el día 2023-04-03

HORIZON-MSCA-2022-PF-01-01: MSCA Postdoctoral Fellowships 2022 ExpectedOutcome:

I+D

Cerrada hace 2 años

0% 100% 100%

Información adicional privada

No hay información privada compartida para este proyecto. Habla con el coordinador.

2 Participantes

TU Delft

254.33K€ | Lider

SOLVGE B.V.

N.D. | Participante

Conecta tu I+D

¿Tienes un proyecto y buscas un partner? Gracias a nuestro motor inteligente podemos recomendarte los mejores socios y ponerte en contacto con ellos. Te lo explicamos en este video

Proyectos interesantes

COCOLIH2T COmposite COnformal LIquid H2 Tank 9M€ Cerrado

PID2021-125659OB-I00 PROTECCIONES AUXETICAS PARA IMPACTOS A ALTA VELOCIDAD DE OBJ... 170K€ Cerrado

CTQ2009-07647 MODELOS Y SIMULACIONES CINETICAS Y DINAMICAS DE REACCIONES E... 47K€ Cerrado

TED2021-131618B-C21 MODELADO DE COMBUSTIBLES DE AVIACION SOSTENIBLES PARA BAJAS... 144K€ Cerrado

DPI2013-41094-R ANALISIS DEL COMPORTAMIENTO DE LAMINADOS CARBONO/EPOXI SOMET... 45K€ Cerrado

PRE2020-093592 CONTRIBUCION A LA AVIACION SOSTENIBLE A TRAVES DE LA OPTIMIZ... 99K€ Cerrado

Duración del proyecto: 32 meses Fecha Inicio: 2023-04-03
Fecha Fin: 2025-12-31

Líder del proyecto

TECHNISCHE UNIVERSITEIT DELFT No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 254K€

Descripción del proyecto "Engineering novel materials and their design optimization using simulation-based tools enable the development of lightweight and sturdy thrusters. In Europe, the development of high-temperature-resistant structural materials for space transportation has gained momentum over the years. This has led to the increased usage of ceramic matrix composite over conventional metal alloys in aerospace applications. Most of the reported works focus on manufacturing cost-effective and lightweight composites, whereas the thermally stable nature of composites has not been fully explored. The Green Charter and European Green Deal promote low-emission forms of transport and emphasize developing sustainable and renewable forms of energy. The adoption of green fuels offers advantages in terms of total life cycle cost reduction, contributing to cheaper space transportation, and environmental impact reduction. Contemporary research innovations have expanded the development of ""green propellants"" for spacecraft in diverse space applications on a global level, primarily for eco-innovation and safety considerations. Studies with ammonium dinitramide, hydrazinium nitroformate with methanol, and ethanol-water are still in the nascent phase whereas H2O2 is delivering state-of-the-art performance to replace conventional hydrazine. This project aims to explore the possibility of developing a 1-100N class thruster made of thermally stable composite (carbon-ceramic) and green bipropellant (H2O2-Kerosene) system for the upper stage to reduce the overall weight, life cycle cost, and environmental impacts without compromising on the performance parameters. This will be researched through a comprehensive blend of multi-physics-based numerical modeling and analysis to generate a highly reliable design and a scale-specific experimental characterization and test rig to yield propellant formulation data corresponding to the state-of-the-art. The proposal will produce high societal, scientific, and economic impacts."

Conecta tu I+D

Entra hoy

¿Olvidé mi contraseña?

Financiación

Empresas

CTIs/Universidades

Proyectos

Investigadores