CORDIS - Risultati della ricerca dell’UE
CORDIS

Retro Propulsion Assisted Landing Technologies

Risultati finali

System Definition Report (DLR)

System Definition Report

Data Management Plan (all Partners)

All Partners will be asked to provide input and details concerning different data formats in use the methods to generate visualise and preserve these data DLR

Flight Dynamics Summary Report (DEIMOS)

Flight Dynamics Summary Report

Data Management Report (all Partners)

This report will provide a summary of all the data generated in the project the formats used and how this data is preserved in medium and long term DLR

Final Report (all Partners)

Final Report

GNC Concept and Assessment Summary Report (DEIMOS)

GNC Concept and Assessment Summary Report

FQ, Stability and Controllability Summary Report (DEIMOS)

FQ Stability and Controllability Summary Report

Mission Requirements Catalogue (DLR)

Mission Requirements Catalogue

Dissemination and Exploitation Plan (all Partners)

An initial plan for the dissemination and exploitation of the project results will be prepared All project Partners will participate in this deliverable CFSE

Financial Report (all Partners)

Financial Report

Dissemination and Exploitation Report (all Partners)

It will summarise all dissemination and communication activities carried out during the duration of the project and will provide the exploitation plan of each Partner CFSE

Pubblicazioni

DEIMOS' R&D on Reusable Launchers' Technologies

Autori: Bonetti, D.; De Zaiacomo, G.; Blanco Arnao, G.; Medici, G.
Pubblicato in: 2020
Editore: Congreso de Ingeniería Espacial
DOI: 10.5281/zenodo.5779174

Konstruktion und Fertigung eines Landebeins für das RETALT Projekt

Autori: Becker, Laura
Pubblicato in: Numero 1, 2022
Editore: MT Aerospace
DOI: 10.5281/zenodo.7027372

Development of a Trowelable TPS Cork Material for Reusable Launch Vehicles

Autori: Paixão, Sofia; Carvalho, João; Hantz, Christian
Pubblicato in: FAR2022, 2022
Editore: ESA
DOI: 10.5281/zenodo.6759712

Aerothermal Databases and CFD Based Load Predictions

Autori: Laureti, Mariasole; Karl, Sebastian; Marwege, Ansgar; Gulhan, Ali
Pubblicato in: FAR2022, 2022
Editore: ESA
DOI: 10.5281/zenodo.6759561

Thermal Characterization of Cork and Ceramics-Based TPS in DLRS Arc-heated Wind Tunnel L2K

Autori: Hantz, Christian; Marwege, Ansar; Paixao, Sofia; Celotti, Luca; Wiśniewska, Maria
Pubblicato in: FAR2022, 2022
Editore: ESA
DOI: 10.5281/zenodo.6759736

CFD Simulations and Wind Tunnel Experiments for Re-usable Launch Vehicles

Autori: Vos, Jan; Charbonnier, Dominique; Marwege, Ansgar; Hantz, Christian; Gulhan, Ali
Pubblicato in: FAR2022, 2022
Editore: ESA
DOI: 10.5281/zenodo.6759393

Mission Engineering for the Recovery and Vertical Landing of an Orbital Launch Vehicle

Autori: De Zaiacomo, Gabriele; Medici, Giovanni; Princi, Alessandro
Pubblicato in: FAR2022, 2022
Editore: ESA
DOI: 10.5281/zenodo.6759589

Key Technologies for Retro Propulsive Vertical Descent and Landing – RETALT – An Overview

Autori: Marwege, A.; Klevanski, J.; Hantz, C.; Kirchheck, D.; Gulhan, A.; Karl, S.; Laureti, M.; De Zaiacomo, G.; Vos, J.B.; Thies, C.; Jevons, M.; Krammer, A.; Lichtenberger, M.; Carvalho, J.; Paixão, S.
Pubblicato in: FAR2022, 2022
Editore: ESA
DOI: 10.5281/zenodo.6783915

Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Wind Tunnel Tests

Autori: J.B. Vos, D. Charbonnier, A. Marwege, A. Gülhan, M. Laureti, S. Karl
Pubblicato in: AIAA Scitech 2022, 2022
Editore: AIAA
DOI: 10.2514/6.2022-1308

Aerodynamic Phenomena of Retro Propulsion Descent and Landing Configurations

Autori: Marwege, Ansgar; Hantz, Christian; Kirchheck, Daniel; Klevanski, Josef; Vos, Jan; Laureti, Mariasole; Karl, Sebastian; Gulhan,Ali
Pubblicato in: FAR2022, 2022
Editore: ESA
DOI: 10.5281/zenodo.6783922

Aerothermal analysis of the RETALT2 vehicle

Autori: Mariasole Laureti; Karl, Sebastian
Pubblicato in: Aerosapce Europe Conference - 10th EUCASS - 9th CEAS, 2023
Editore: EUCASS
DOI: 10.5281/zenodo.7983826

Retro Propulsion Assisted Landing Technologies (RETALT): Current Status and Outlook of the EU funded project on Reusable Launch Vehicles

Autori: A. Marwege, A. Guelhan, J. Klevanski, J. Riehmer, S. Karl, D. Kirchheck, D. Bonetti, J. Vos, M. Jevons, A. Krammer, J. Carvalho
Pubblicato in: 70th International Astronautical Congress (IAC), 2019
Editore: IAF
DOI: 10.5281/zenodo.5770046

Design and Manufacturing Status of Advanced Structures for Reusable Launch Systems Demonstrators with Retro Propulsion Assisted Landing Technologies (RETALT)

Autori: P. Starke, C. Dorbath, D. Zell
Pubblicato in: 70th International Astronautical Congress (IAC), 2019
Editore: IAF
DOI: 10.5281/zenodo.5770094

RETALT - RETro propulsion Assisted Landing Technologies

Autori: A. Guelhan, A. Marwege, J. Klevanski, S. Karl, D. Bonetti, J. Vos, M. Jevons, A. Krammer, J. Carvalho
Pubblicato in: Internation Plenatry Probe Workshop, 2019
Editore: IPPW
DOI: 10.5281/zenodo.5770145

Design and Manufacturing Status of Advanced Structures for Reusable Launch Systems Demonstrators with Retro Propulsion Assisted Landing Technologies (RETALT)

Autori: P. Starke, C. Dorbath
Pubblicato in: EUCASS, 2019
Editore: EUCASS
DOI: 10.5281/zenodo.5779163

Drop Test Description and Evaluation of a Landing Leg for a Re-usable Future Launche Vehicle

Autori: Thies, Christoph
Pubblicato in: FAR2022, 2022
Editore: ESA
DOI: 10.5281/zenodo.6759766

RETALT: Development of Key Flight Dynamics and GNC Technologies for Reusable Launchers

Autori: De Zaiacomo, G.; Medici, G.; Princi, A.; Ghignoni, P.; Botelho, A.; Martinez Arlandis, M.; Recupero,C.; Fabrizi, A.; Fernandez, F.; Guidotti, G.
Pubblicato in: IAC 2022 Conference, Numero 1, 2022
Editore: IAC
DOI: 10.5281/zenodo.7064630

Landing Leg and Aerodynamic Control Surface Mechanisms and Functional Demonstrators for the RETALT1 Launch Vehicle

Autori: Krammer, Anett; Nebuloni, Stefano; Lichtenberger, Marc
Pubblicato in: FAR2022, 2022
Editore: ESA
DOI: 10.5281/zenodo.6759777

Optimum GNC Solutions for the Recovery and Vertical Landing of an Orbital Launch Vehicle

Autori: Martinez, Marc; Ghignoni, Pietro; Botelho, Afonso; Recupero, Cristina; Fabrizi, Andrea; Fernandez, Vincente; De Zaiacomo, Gabriele
Pubblicato in: FAR2022, 2022
Editore: ESA
DOI: 10.5281/zenodo.6759659

RETALT: Recovery GNC for the Retro-Propulsive Vertical Landing of an Orbital Launch Vehicle

Autori: Ghignoni, P.; Botelho, A.; Recupero, C.; Fernandez, V.; Fabrizi, A.; De Zaiacomo, G.
Pubblicato in: HiSST Conference, Numero 1, 2022
Editore: HiSST Organizers
DOI: 10.5281/zenodo.7064613

RETALT: Development of an Optimal GNC Solution for Recovery of an Orbital Launch Vehicle

Autori: Botelho, A.; Recupero, C.; Fernandez, V.; Fabrizi, A.; De Zaiacomo, G.
Pubblicato in: ICATT, 2021
Editore: International Conference on Astrodynamics Tools and Techniques
DOI: 10.5281/zenodo.5779496

TPS Design and Manufacturing for the RETALT VTVL launcher

Autori: João Carvalho, Cládia Peixoto, Marta Reinas, Sofia Paixão
Pubblicato in: CEAS Space Journal, 2022, ISSN 1868-2510
Editore: Springer
DOI: 10.1007/s12567-021-00417-w

Hypersonic retro propulsion for reusable launch vehicles tested in the H2K wind tunnel

Autori: Marwege, Ansgar; Kirchheck, Daniel; Klevanski, Josef; Gulhan, Ali
Pubblicato in: CEAS Space Journal, 2022, ISSN 1868-2510
Editore: Springer
DOI: 10.1007/s12567-022-00457-w

Investigation of the landing dynamics of a reusable launch vehicle and derivation of dimension loading for the landing leg

Autori: Thies, Christoph
Pubblicato in: CEAS Space Journal, Numero 1, 2022, ISSN 1868-2502
Editore: Springer Verlag
DOI: 10.1007/s12567-022-00456-x

Computational fluid dynamics investigations of aerodynamic control surfaces of a vertical landing configuration

Autori: Charbonnier, Dominique; Vos, Jan; Marwege, Ansgar; Hantz, Christian
Pubblicato in: CEAS Space Journal, Numero 2, 2022, ISSN 1868-2510
Editore: Springer
DOI: 10.1007/s12567-022-00431-6

Unsteady Aerodynamics of the Retropropulsion Reentry Burn of Vertically Landing Launchers

Autori: Marwege, A.; Gülhan, A.
Pubblicato in: AIAA Journal of Spacecraft and Rockets, Numero 4, 2023, ISSN 1533-6794
Editore: AIAA
DOI: 10.2514/1.A35647

Mission Engineering for the RETALT VTVL launcher

Autori: Gabriele De Zaiacomo, Gonzalo Blanco Arnao, Riccardo Bunt, Davide Bonetti
Pubblicato in: CEAS Space Journal, 2022, ISSN 1868-2510
Editore: Springer
DOI: 10.1007/s12567-021-00415-y

RETALT: review of technologies and overview of design changes

Autori: Marwege, Ansgar; Gülhan, Ali; Klevanski, Josef; Hantz, Christian; Karl, Sebastian; Laureti, Mariasole; De Zaiacomo, Gabriele; Vos, Jan; Jevons, Matthew; Thies, Christoph; Krammer, Anett; Lichtenberger, Marc; Carvalho, João; Paixão, Sofia
Pubblicato in: CEAS Space Journal, 2022, ISSN 1868-2510
Editore: Springer
DOI: 10.1007/s12567-022-00458-9

Wind Tunnel Experiments of Interstage Segments used for Aerodynamic Control of Retro-Propulsion Assisted Landing Vehicles (RETALT)

Autori: Ansgar Marwege, Christian Hantz, Daniel Kirchcheck, Dominique Charbonnier, Jan Vos, Josef Klevanski, Ali Gülhan
Pubblicato in: CEAS Space Journal, 2022, ISSN 1868-2510
Editore: Springer
DOI: 10.1007/s12567-022-00425-4

Retro propulsion assisted landing technologies: the RETALT project

Autori: Gülhan, Ali; Marwege, Ansgar; Vos, Jan
Pubblicato in: CEAS Space Journal, 2022, ISSN 1868-2510
Editore: Springer
DOI: 10.1007/s12567-022-00460-1

Fin actuation, thrust vector control and landing leg mechanisms design for the RETALT VTVL launcher

Autori: Anett Krammer, Marc Lichtenberger, Luc Blecha
Pubblicato in: CEAS Space Journal, 2022, ISSN 1868-2510
Editore: Springer
DOI: 10.1007/s12567-021-00421-0

Aerothermal databases and load predictions for Retro Propulsion-Assisted Launch Vehicles (RETALT)

Autori: Laureti, Mariasole; Karl, Sebastian
Pubblicato in: CEAS Space Journal, 2022, ISSN 1868-2510
Editore: Springer
DOI: 10.1007/s12567-021-00413-0

Design of the Return GNC solution for the Retro-Propulsive Vertical Landing of RETALT

Autori: Afonso Botelho, Marc Martinez, Cristina Recupero, Andrea Fabrizi, Gabriele De Zaiacomo
Pubblicato in: CEAS Space Journal, 2022, ISSN 1868-2510
Editore: Springer
DOI: 10.1007/s12567-022-00423-6

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