Hybrid Propulsion Module for transfer to GEO orbit

Project Information

HYPROGEO

Grant agreement ID: 634534

DOI 10.3030/634534

Project closed

EC signature date 17 November 2014

Start date 1 February 2015

End date 31 January 2018

Funded under

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

Total cost € 2 993 888,00

EU contribution € 2 993 888,00

Coordinated by

AIRBUS DEFENCE AND SPACE SAS
France

Deliverables

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

Author(s): 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
Published in: EUCASS17, 2017
Publisher: 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

Author(s): J-Y. Lestrade , J. Anthoine, A. J. Musker, M. Faenza3 and A. Lecossais
Published in: Space Propulsion 2018, 2018
Publisher: ESA

Catalytic Injectors for an Isochoric Hybrid Rocket Motor

Author(s): Antony J. Musker, Jean-Yves Lestrade, Jérôme Anthoine, Anthony Lécossais
Published in: Space Propulion 2018, 2018
Publisher: ESA

HYPROGEO Hybrid Propulsion: Latest project achievements

Author(s): Lécossais , Anthony; Odic , Karine; Fiot , Daniel; Lestrade , Jean-Yves; Verberne , Onno; Fernando , Priya; Christ , Philipp; Searle , Tim
Published in: Space Propulsion 2018, May 2018, SEVILLE, Spain, Issue 1, 2018
Publisher: Space Propulsion Conference

HYPROGEO Hybrid Propulsion: Potential Applications & Technical Challenges

Author(s): 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
Published in: SPACE PROPULSION 2016, 2016
Publisher: 3AF

Realistic Testing of PX1 Catalyst Using Near-Anhydrous Hydrogen Peroxide

Author(s): 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
Published in: SPACE PROPULSION 2016, 2016
Publisher: 3AF

HYPROGEO Hybrid Propulsion: Project Objectives and Coordination

Author(s): Odic K., Lestrade J.-Y., Verbene O., Ryan J., Christ P., de Crombrugghe G.
Published in: Space Propulsion 2016, 2016
Publisher: 3AF

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

Author(s): Faenza M. & al.
Published in: SPACE PROPULSION 2016, 2016
Publisher: 3AF

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

Author(s): J-Y. Lestrade, J. Anthoine, H. Bavestrello, A. Lecossais, F. Barato and J-B. Gouriet
Published in: SPACE PROPULSION 2016, 2016
Publisher: 3AF

Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion

Author(s): 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]
Published in: Space Propulsion 2016, 2016
Publisher: 3AF

Other (1)

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

Author(s): Macdonald M., Owens S.
Published in: Acta Astronautica, 2016
Publisher: Acta Astronautica