Opendata, web and dolomites

HYPROGEO

Hybrid Propulsion Module for transfer to GEO orbit

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

0

Project "HYPROGEO" data sheet

The following table provides information about the project.

Coordinator
AIRBUS DEFENCE AND SPACE SAS 

Organization address
address: 31 RUE DES COSMONAUTES ZI DU PALAYS
city: TOULOUSE CEDEX
postcode: 31402
website: www.airbusdefenceandspace.com

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 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

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    AIRBUS DEFENCE AND SPACE SAS FR (TOULOUSE CEDEX) coordinator 740˙277.00
2    OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES FR (PALAISEAU) participant 512˙693.00
3    NAMMO RAUFOSS AS NO (RAUFOSS) participant 301˙303.00
4    SPACETEC PARTNERS SPRL BE (BRUXELLES) participant 200˙000.00
5    UNIVERSITA DEGLI STUDI DI PADOVA IT (PADOVA) participant 199˙027.00
6    DELTACAT Limited UK (Lee-on-Solent, Hampshire) participant 186˙291.00
7    EVONIK RESOURCE EFFICIENCY GMBH DE (ESSEN) participant 176˙254.00
8    NAMMO WESTCOTT LTD UK (AYLESBURY) participant 121˙215.00
9    SIEC BADAWCZA LUKASIEWICZ-INSTYTUTLOTNICTWA PL (WARSZAWA) participant 113˙625.00
10    AIRBUS DEFENCE AND SPACE LTD UK (STEVENAGE) participant 108˙250.00
11    INSTITUT VON KARMAN DE DYNAMIQUE DES FLUIDES BE (RHODE SAINT GENESE) participant 80˙000.00
12    AIRBUS DEFENCE AND SPACE GMBH DE (TAUFKIRCHEN) participant 77˙943.00
13    ARIANEGROUP GMBH DE (TAUFKIRCHEN) participant 72˙056.00
14    UNIVERSITY OF STRATHCLYDE UK (GLASGOW) participant 50˙405.00
15    ARIANEGROUP SAS FR (PARIS) participant 30˙800.00
16    EVONIK INDUSTRIES AG DE (ESSEN) participant 23˙745.00
17    AIRBUS DS GMBH DE (TAUFKIRCHEN) participant 0.00

Map

 Project objective

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.

 Deliverables

List of deliverables.
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.

 Publications

year authors and title journal last update
List of publications.
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

Are you the coordinator (or a participant) of this project? Plaese send me more information about the "HYPROGEO" project.

For instance: the website url (it has not provided by EU-opendata yet), the logo, a more detailed description of the project (in plain text as a rtf file or a word file), some pictures (as picture files, not embedded into any word file), twitter account, linkedin page, etc.

Send me an  email (fabio@fabiodisconzi.com) and I put them in your project's page as son as possible.

Thanks. And then put a link of this page into your project's website.

The information about "HYPROGEO" are provided by the European Opendata Portal: CORDIS opendata.

More projects from the same programme (H2020-EU.2.1.6.1.)

Go2Space-HUBs (2019)

Generating new sOlutions 2 and from Space through effective local start-up HUBs

Read More  

FALCon (2019)

Formation flight for in-Air Launcher 1st stage Capturing demonstration

Read More  

CopHub.AC (2018)

Copernicus Academy Hub for Knowledge, Innovation and Outreach

Read More