Explore the words cloud of the HYPROGEO project. It provides you a very rough idea of what is the project "HYPROGEO" about.
The following table provides information about the project.
Coordinator |
AIRBUS DEFENCE AND SPACE SAS
Organization address contact info |
Coordinator Country | France [FR] |
Project website | https://www.hyprogeo.eu/ |
Total cost | 2˙993˙888 € |
EC max contribution | 2˙993˙888 € (100%) |
Programme |
1. H2020-EU.2.1.6.1. (Enabling European competitiveness, non-dependence and innovation of the European space sector) |
Code Call | H2020-COMPET-2014 |
Funding Scheme | RIA |
Starting year | 2015 |
Duration (year-month-day) | from 2015-02-01 to 2018-01-31 |
Take a look of project's partnership.
Independent access to space is a key component of the European Space Policy. The competition is increasing in this area both for the full launching systems and the key subsystems. Cost-effectiveness becomes the main driving factor. HYPROGEO ambition is to study a propulsion module based on Hybrid chemical propulsion. Hybrid propulsion is not a new technology but its application to a transfer module or to a re-ignitable upper stage is very innovative. It is an interesting alternative for the GEO transfer, between the chemical propulsion (bi-liquid) and the new trend of Electrical Propulsion (EP). There are very good synergies and complementarities with the other propulsion activities. The proof of concept (specific impulse, thrust) has been demonstrated. The main technical challenge is the long duration firings. The future development of an operational system, already identified in the current roadmaps, requires advanced R&D work on 4 critical technologies: - Combustion chamber. - High endurance nozzle. - Catalytic injector. - Production, storage and use of high concentration hydrogen peroxide.
These R&D activities structure 4 main work packages. A system study ensures the global vision in coherence with an economic analysis, the identification of technical challenges and the consolidation of scientific results. A last work package performs the dissemination of results. An innovative aspect is the fact that the R&D activities are directly driven by the ecvolution of market needs and system requirements. Main expected benefits are: - Green and simpler design (compared to bi-liquid). - Shorter transfer time and reduced cost of operations (compared to EP)
A TRL 3-4 level is expected at the end of the project. The impact of the project is secured by the composition of the consortium led by Astrium with the main European actors of the hybrid: it contributes to the consolidation of the European industrial supply chain for Hybrid propulsion. Project duration is 36 months.
Project Brochure V2 and Project Video V1 | Websites, patent fillings, videos etc. | 2019-05-30 15:42:48 |
Project video - Version 2 | Websites, patent fillings, videos etc. | 2019-05-30 15:42:48 |
Dissemination Report (V2) | Documents, reports | 2019-05-30 15:42:48 |
Dissemination Report (V3) | Documents, reports | 2019-05-30 15:42:48 |
Communication Strategy and Action Plan: defines targets, messages, tools and timeline. | Documents, reports | 2019-05-30 15:42:48 |
Public Website and project brochure V1 | Websites, patent fillings, videos etc. | 2019-05-30 15:42:48 |
Dissemination Report (V1) | Documents, reports | 2019-05-30 15:42:48 |
Take a look to the deliverables list in detail: detailed list of HYPROGEO deliverables.
year | authors and title | journal | last update |
---|---|---|---|
2017 |
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 Development and test of an innovative Hybrid rocket combustion chamber published pages: , ISSN: , DOI: 10.13009/EUCASS2017-414 |
EUCASS17 | 2019-06-03 |
2018 |
Antony J. Musker, Jean-Yves Lestrade, Jérôme Anthoine, Anthony Lécossais Catalytic Injectors for an Isochoric Hybrid Rocket Motor published pages: , ISSN: , DOI: |
Space Propulion 2018 | 2019-06-03 |
2018 |
J-Y. Lestrade , J. Anthoine, A. J. Musker, M. Faenza3 and A. Lecossais Experimental Demonstration of an Innovative Hybrid Rocket Engine Compatible with Long Duration Operation published pages: , ISSN: , DOI: |
Space Propulsion 2018 | 2019-06-03 |
2018 |
Lécossais , Anthony; Odic , Karine; Fiot , Daniel; Lestrade , Jean-Yves; Verberne , Onno; Fernando , Priya; Christ , Philipp; Searle , Tim HYPROGEO Hybrid Propulsion: Latest project achievements published pages: , ISSN: , DOI: |
Space Propulsion 2018, May 2018, SEVILLE, Spain 1 | 2019-05-30 |
2016 |
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) francesco.barato@unipd.it, (2) Jean-Yves.Lestrade@onera.fr Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion published pages: , ISSN: , DOI: |
Space Propulsion 2016 | 2019-06-03 |
2016 |
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 SG1 2AS, UK
(4) University of Strathclyde, Glasgow G1 1XJ, Scotland
(5) SpaceTec Partners, Avenue Louise 66, 1050 Brussels, Belgium HYPROGEO Hybrid Propulsion: Potential Applications & Technical Challenges published pages: , ISSN: , DOI: |
SPACE PROPULSION 2016 | 2019-06-03 |
2016 |
J-Y. Lestrade, J. Anthoine, H. Bavestrello, A. Lecossais, F. Barato and J-B. Gouriet Achieving long duration and constant thrust with hybrid rocket combustion chamber for spacecraft application published pages: , ISSN: , DOI: |
SPACE PROPULSION 2016 | 2019-06-03 |
2016 |
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,
tony.musker@deltacatuk.com
2 Airbus Defence and Space Ltd, Gunnels Wood Road, Stevenage, Hertfordshire, SG1 2AS, UK,
julia.ryan@airbus.com
3 Institute of Aviation (IOA, Instytut Lotnictwa), Al. Krakowska 110/114, 02-256 Warsaw, Poland,
wojciech.florczuk@ilot.edu.pl
4 Evonik Resource Efficiency GmbH, Rodenbacher Chaussee 4, 63457 Hanau-Wolfgang, Germany,
philipp.christ@evonik.com Realistic Testing of PX1 Catalyst Using Near-Anhydrous Hydrogen Peroxide published pages: , ISSN: , DOI: |
SPACE PROPULSION 2016 | 2019-06-03 |
2016 |
Odic K., Lestrade J.-Y., Verbene O., Ryan J., Christ P., de Crombrugghe G. HYPROGEO Hybrid Propulsion: Project Objectives and Coordination published pages: , ISSN: , DOI: |
Space Propulsion 2016 | 2019-06-03 |
2016 |
Faenza M. & al. C/C-SiC Nozzle for a Long Burn-Time Hybrid Rocket: Design and Optimization, Manufacturing and Testing published pages: , ISSN: , DOI: |
SPACE PROPULSION 2016 | 2019-06-03 |
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