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Hybrid Rocket Technology Exploration

The space industry is going through a transformational phase, creating unprecedented levels of growth for space and nonspace actors/industry. In the next years a significant increase in the market of small satellites up to 500 kg... ver más

28/02/2023

HYIMPULSE

175K€

Presupuesto del proyecto: 175K€

Líder del proyecto

HYIMPULSE TECHNOLOGIES GMBH No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Fecha límite participación Sin fecha límite de participación.

Financiación concedida El organismo H2020 notifico la concesión del proyecto el día 2023-02-28

MSCA-IF-2020: Individual Fellowships

I+D

Cerrada hace 4 años

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Información adicional privada

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

1 Participantes

HYIMPULSE

174.81K€ | Lider

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Duración del proyecto: 24 meses Fecha Inicio: 2021-02-23
Fecha Fin: 2023-02-28

Líder del proyecto

HYIMPULSE TECHNOLOGIES GMBH No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 175K€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto The space industry is going through a transformational phase, creating unprecedented levels of growth for space and nonspace actors/industry. In the next years a significant increase in the market of small satellites up to 500 kg is expected. The HyImpulse start-up has been created recently and intends to bring to the market the key technologies for a game-changing, unique, low risk, innovative small launcher, with a 500 kg payload capability to LEO. The launcher will be based on a combination of novel and established technologies, using inherently safe hybrid propulsion (paraffin/LOX propellants). These engines combine a liquid oxidizer with a solid fuel thus enabling to benefit from both bi-liquid and solid technologies and advantages. Unlike solid and liquid technologies, hybrid engines did not benefit from large investments and research in the past due to the inherent complex phenomena occurring into their combustion chamber. This is however changing with the new space constraints which make hybrid motors serious candidate for future applications. This research fellowship aims at bringing hybrid propulsion from the current state of development to a fully mature technology enabling the flight of sounding rockets and small launchers. The action will allow the elaboration of novel measurement and analysis techniques to study the fuel regression rate, the wax composition properties & the engine performances and stability. In addition to the scientific investigations of complex and coupled phenomena occurring in the combustion chamber of a hybrid engine, an innovative wax manufacturing process will be optimised in collaboration with colleagues from HyImpulse. The most original aspect of the fellowship is the combination of scientific investigations of complex phenomena with innovative technical developments that are required to make hybrid propulsion technology competitive in the coming years.

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