Hola,
¿eres nuevo aquí?

Registrate y conecta tu empresa con financiación pública, partners y proyectos.

HYPER-CAT

Financiado

Utilization of H2O2 in Transpiration Cooling System for Active Heat Protection a...

Utilization of H2O2 in Transpiration Cooling System for Active Heat Protection and Implementation of Thermal Decomposition for Catalyst Free H2O2/Kerosene Bipropellant Aerospike Rocket Engin The rapid increase in the number of small satellites in recent years has dramatically boosted the probability of orbital collisions that inevitably create space debris. To preserve the orbit's sustainability, a storable/stable, en... ver más

12/05/2026

TUD

190K€

Presupuesto del proyecto: 190K€

Líder del proyecto

TECHNISCHE UNIVERSITAET DRESDEN No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Ver 1 Participantes

Financiación concedida El organismo HORIZON EUROPE notifico la concesión del proyecto el día 2023-07-10

Línea de financiación objetivo El proyecto se financió a través de la siguiente ayuda:

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

I+D

Cerrada hace 2 años

0% 100%

1 Participantes

TUD

189.69K€ | Lider

Proyectos interesantes

TED2021-132484B-I00 PROPELENTES SOSTENIBLES PARA MOTORES DE PLASMA EN ORBITA TER... 111K€ Cerrado

AYA2012-34131 GESTION DE FLUJOS MULTIFASICOS Y DE ENERGIA PARA APLICACIONE... 140K€ Cerrado

GREENLAM Lightweight, Cost-effective Composite and Green Bipropellant... 254K€ Cerrado

EMBRACE II Ramping up production capacity of groundbreaking space propu... 4M€ Cerrado

CRYSALIS Cryogenic storage and refuelling in space 7M€ Cerrado

REDECORATE REcommissioning and DEorbiting using Cubesat swarms with ele... 289K€ Cerrado

Últimas noticias

27-11-2024: Videojuegos y creaci... Se abre la línea de ayuda pública: Ayudas para la promoción del sector del videojuego, del pódcast y otras formas de creación digital

27-11-2024: DGIPYME En las últimas 48 horas el Organismo DGIPYME ha otorgado 1 concesiones

27-11-2024: FUNDACION-EOI En las últimas 48 horas el Organismo FUNDACION EOI ha otorgado 2 concesiones

Duración del proyecto: 34 meses Fecha Inicio: 2023-07-10
Fecha Fin: 2026-05-12

Líder del proyecto

TECHNISCHE UNIVERSITAET DRESDEN

TRL 4-5

Presupuesto del proyecto 190K€

Descripción del proyecto The rapid increase in the number of small satellites in recent years has dramatically boosted the probability of orbital collisions that inevitably create space debris. To preserve the orbit's sustainability, a storable/stable, environmentally-friendly, highly efficient, and compact propulsion system is required to be mounted on the satellites. Hydrogen Peroxide (H2O2) and aerospike engines are promising candidates if the major flaws are solved: catalyst performance degradation due to stabilizer poisoning and extreme thermal loads at the spike structure. In this proposal, I want to test the novel concept of utilizing the thermal decomposition process of H2O2 by turning the aerospike engine's cooling challenges into an advantage. Liquid H2O2 adsorbs heat from the structure convectively, then vaporizes/decomposes to create gas layers to protect the structure from the direct contact of the combustion gas. The thermal decomposition of H2O2 eliminates the use of catalysts. Overall, the concept offers a unique approach to an efficient, compact, and durable propulsion system for small satellites. In the project, liquid H2O2 will be injected into the H2O2/Kerosene staged-combustion vitiated-air heater through the additive manufactured porous metallic wall (Fraunhofer IWS). Testing in various conditions, heat flux/temperature/pressure will be measured directly. Key variables (Da and H*) can't be directly measured. Hence, the mathematical model will be formulated to derive these variables under given conditions. The model will be validated by comparing the mono/bipropellant flame front locations between the simulations/experiments. Then, I will generate a low-order modeling tool that can predict the cooling performance and combustion efficiency based on the data and the model. The tool will be implemented to apply the new concept to existing TUD etholox rockets. The spike module will be fabricated, integrated and tested for concept verification.

Conecta tu I+D

Entra hoy

Financiación

Empresas

CTIs/Universidades

Proyectos

Investigadores