Hybrid Propulsion Module for transfer to GEO orbit

Información del proyecto

HYPROGEO

Identificador del acuerdo de subvención: 634534

DOI

10.3030/634534

Proyecto cerrado

Fecha de la firma de la CE 17 Noviembre 2014

Fecha de inicio 1 Febrero 2015

Fecha de finalización 31 Enero 2018

Financiado con arreglo a

• INDUSTRIAL LEADERSHIP - Leadership in enabling and industrial technologies – Space

Coste total

€ 2 993 888,00

Aportación de la UE

€ 2 993 888,00

Coordinado por

AIRBUS DEFENCE AND SPACE SAS
France

CORDIS proporciona enlaces a los documentos públicos y las publicaciones de los proyectos de los programas marco HORIZONTE.

Los enlaces a los documentos y las publicaciones de los proyectos del Séptimo Programa Marco, así como los enlaces a algunos tipos de resultados específicos, como conjuntos de datos y «software», se obtienen dinámicamente de OpenAIRE .

Resultado final

Documents, reports (4)

Dissemination Report (V2)

Dissemination Report (second release) with a list of all activities performed and copies of all dissemination material produced between M12 and M24.

Communication Strategy and Action Plan: defines targets, messages, tools and timeline.
Dissemination Report (V1)

Dissemination Report (first release) with a list of all activities performed and copies of all dissemination material produced (between kick-off and M12).

Dissemination Report (V3)

Dissemination Report (third and final release) with a list of all activities performed and copies of all dissemination material produced (between M24 and M36).

Websites, patent fillings, videos etc. (3)

Public Website and project brochure V1
Project Brochure V2 and Project Video V1

Project Brochure V2 and Project Video V1 (with update at M30)

Project video - Version 2

Second and final version of the project video, updated with firing tests, demonstrations and results

Publicaciones

Conference proceedings (10)

Development and test of an innovative Hybrid rocket combustion chamber

Autores: J-Y. Lestrade*, J. Messineo*, J. Anthoine*, A. Musker** and F. Barato*** *ONERA – The French Aerospace Lab F-31410 Mauzac, France **DELTACAT Ltd Kintyre House, 70 High Street Fareham, PO16 7BB, UK ***Department of Industrial Engineering, University of Padova Via Venezia 59/4 35131 Padova, Italy
Publicado en: EUCASS17, 2017
Editor: 7th European Conference for Aeronautics and Space Sciences
DOI: 10.13009/EUCASS2017-414

Experimental Demonstration of an Innovative Hybrid Rocket Engine Compatible with Long Duration Operation

Autores: J-Y. Lestrade , J. Anthoine, A. J. Musker, M. Faenza3 and A. Lecossais
Publicado en: Space Propulsion 2018, 2018
Editor: ESA

Catalytic Injectors for an Isochoric Hybrid Rocket Motor

Autores: Antony J. Musker, Jean-Yves Lestrade, Jérôme Anthoine, Anthony Lécossais
Publicado en: Space Propulion 2018, 2018
Editor: ESA

HYPROGEO Hybrid Propulsion: Latest project achievements

Autores: Lécossais , Anthony; Odic , Karine; Fiot , Daniel; Lestrade , Jean-Yves; Verberne , Onno; Fernando , Priya; Christ , Philipp; Searle , Tim
Publicado en: Space Propulsion 2018, May 2018, SEVILLE, Spain, Edición 1, 2018
Editor: Space Propulsion Conference

HYPROGEO Hybrid Propulsion: Potential Applications & Technical Challenges

Autores: Anthony Lécossais(1), Henri Bavestrello(1), Karine Odic(1), Fanny Ducerf (2), Fabrice Martin (2), Julia Ryan(3), Malcolm Macdonald(4), Guerric de Crombrugghe(5) (1)Airbus Defence and Space SAS, 31 rue des cosmonautes, 31400 Toulouse, France (2)Airbus Defence and Space SAS, 61 route de Verneuil, 78130 Les Mureaux, France (3)Airbus Defence and Space Ltd, Gunnels Wood Rd, Stevenage, Hertfordshire SG
Publicado en: SPACE PROPULSION 2016, 2016
Editor: 3AF

Realistic Testing of PX1 Catalyst Using Near-Anhydrous Hydrogen Peroxide

Autores: Antony J. Musker1, Julia Ryan2, Wojciech Florczuk3, Kamil Sobczak3, Damian Kaniewski3, Grzegorz Rarata3, Stefan Leininger4, Philipp Christ4 1 DELTACAT Ltd, Kintyre House, 70 High Street, Fareham, Hampshire, PO16 7BB, UK, [e-mail] 2 Airbus Defence and Space Ltd, Gunnels Wood Road, Stevenage, Hertfordshire, SG1 2AS, UK, [e-mail] 3 Institute of Aviation (IOA, Instytut L
Publicado en: SPACE PROPULSION 2016, 2016
Editor: 3AF

HYPROGEO Hybrid Propulsion: Project Objectives and Coordination

Autores: Odic K., Lestrade J.-Y., Verbene O., Ryan J., Christ P., de Crombrugghe G.
Publicado en: Space Propulsion 2016, 2016
Editor: 3AF

C/C-SiC Nozzle for a Long Burn-Time Hybrid Rocket: Design and Optimization, Manufacturing and Testing

Autores: Faenza M. & al.
Publicado en: SPACE PROPULSION 2016, 2016
Editor: 3AF

Achieving long duration and constant thrust with hybrid rocket combustion chamber for spacecraft application

Autores: J-Y. Lestrade, J. Anthoine, H. Bavestrello, A. Lecossais, F. Barato and J-B. Gouriet
Publicado en: SPACE PROPULSION 2016, 2016
Editor: 3AF

Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion

Autores: F. Barato (1), E. Paccagnella (1), G. Venturelli (1), M. Scarpa (1), F. Picano (1), D. Pavarin (1), and J-Y. Lestrade (2) (1) Dipartimento di Ingegneria Industriale, Università degli Studi di Padova, Via Venezia 1, 35131, Padova, Italy (2) Onera, The French Aerospace Lab, F31410, Mauzac, France (1) [e-mail], (2) [e-mail]
Publicado en: Space Propulsion 2016, 2016
Editor: 3AF

Other (1)

Combined High and Low-Thrust Geostationary Orbit Insertion with Radiation Constraint

Autores: Macdonald M., Owens S.
Publicado en: Acta Astronautica, 2016
Editor: Acta Astronautica