Hybrid Propulsion Module for transfer to GEO orbit

Informations projet

HYPROGEO

N° de convention de subvention: 634534

DOI

10.3030/634534

Projet clôturé

Date de signature de la CE 17 Novembre 2014

Date de début 1 Février 2015

Date de fin 31 Janvier 2018

Financé au titre de

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

Coût total

€ 2 993 888,00

Contribution de l’UE

€ 2 993 888,00

Coordonné par

AIRBUS DEFENCE AND SPACE SAS
France

CORDIS fournit des liens vers les livrables publics et les publications des projets HORIZON.

Les liens vers les livrables et les publications des projets du 7e PC, ainsi que les liens vers certains types de résultats spécifiques tels que les jeux de données et les logiciels, sont récupérés dynamiquement sur OpenAIRE .

Livrables

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

Publications

Conference proceedings (10)

Development and test of an innovative Hybrid rocket combustion chamber

Auteurs: 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
Publié dans: EUCASS17, 2017
Éditeur: 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

Auteurs: J-Y. Lestrade , J. Anthoine, A. J. Musker, M. Faenza3 and A. Lecossais
Publié dans: Space Propulsion 2018, 2018
Éditeur: ESA

Catalytic Injectors for an Isochoric Hybrid Rocket Motor

Auteurs: Antony J. Musker, Jean-Yves Lestrade, Jérôme Anthoine, Anthony Lécossais
Publié dans: Space Propulion 2018, 2018
Éditeur: ESA

HYPROGEO Hybrid Propulsion: Latest project achievements

Auteurs: Lécossais , Anthony; Odic , Karine; Fiot , Daniel; Lestrade , Jean-Yves; Verberne , Onno; Fernando , Priya; Christ , Philipp; Searle , Tim
Publié dans: Space Propulsion 2018, May 2018, SEVILLE, Spain, Numéro 1, 2018
Éditeur: Space Propulsion Conference

HYPROGEO Hybrid Propulsion: Potential Applications & Technical Challenges

Auteurs: 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
Publié dans: SPACE PROPULSION 2016, 2016
Éditeur: 3AF

Realistic Testing of PX1 Catalyst Using Near-Anhydrous Hydrogen Peroxide

Auteurs: 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
Publié dans: SPACE PROPULSION 2016, 2016
Éditeur: 3AF

HYPROGEO Hybrid Propulsion: Project Objectives and Coordination

Auteurs: Odic K., Lestrade J.-Y., Verbene O., Ryan J., Christ P., de Crombrugghe G.
Publié dans: Space Propulsion 2016, 2016
Éditeur: 3AF

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

Auteurs: Faenza M. & al.
Publié dans: SPACE PROPULSION 2016, 2016
Éditeur: 3AF

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

Auteurs: J-Y. Lestrade, J. Anthoine, H. Bavestrello, A. Lecossais, F. Barato and J-B. Gouriet
Publié dans: SPACE PROPULSION 2016, 2016
Éditeur: 3AF

Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion

Auteurs: 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]
Publié dans: Space Propulsion 2016, 2016
Éditeur: 3AF

Other (1)

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

Auteurs: Macdonald M., Owens S.
Publié dans: Acta Astronautica, 2016
Éditeur: Acta Astronautica