Retro Propulsion Assisted Landing Technologies

Resultado final

System Definition Report

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

Press Release, project logo, templates for presentations and reports (CFSE)

Press Release project logo templates for presentations and reports

Publicaciones

DEIMOS' R&D on Reusable Launchers' Technologies

Autores: Bonetti, D.; De Zaiacomo, G.; Blanco Arnao, G.; Medici, G.
Publicado en: 2020
Editor: Congreso de Ingeniería Espacial
DOI: 10.5281/zenodo.5779174

Konstruktion und Fertigung eines Landebeins für das RETALT Projekt

Autores: Becker, Laura
Publicado en: Edición 1, 2022
Editor: MT Aerospace
DOI: 10.5281/zenodo.7027372

Development of a Trowelable TPS Cork Material for Reusable Launch Vehicles

Autores: Paixão, Sofia; Carvalho, João; Hantz, Christian
Publicado en: FAR2022, 2022
Editor: ESA
DOI: 10.5281/zenodo.6759712

Aerothermal Databases and CFD Based Load Predictions

Autores: Laureti, Mariasole; Karl, Sebastian; Marwege, Ansgar; Gulhan, Ali
Publicado en: FAR2022, 2022
Editor: ESA
DOI: 10.5281/zenodo.6759561

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

Autores: Hantz, Christian; Marwege, Ansar; Paixao, Sofia; Celotti, Luca; Wiśniewska, Maria
Publicado en: FAR2022, 2022
Editor: ESA
DOI: 10.5281/zenodo.6759736

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

Autores: Vos, Jan; Charbonnier, Dominique; Marwege, Ansgar; Hantz, Christian; Gulhan, Ali
Publicado en: FAR2022, 2022
Editor: ESA
DOI: 10.5281/zenodo.6759393

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

Autores: De Zaiacomo, Gabriele; Medici, Giovanni; Princi, Alessandro
Publicado en: FAR2022, 2022
Editor: ESA
DOI: 10.5281/zenodo.6759589

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

Autores: 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.
Publicado en: FAR2022, 2022
Editor: ESA
DOI: 10.5281/zenodo.6783915

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

Autores: J.B. Vos, D. Charbonnier, A. Marwege, A. Gülhan, M. Laureti, S. Karl
Publicado en: AIAA Scitech 2022, 2022
Editor: AIAA
DOI: 10.2514/6.2022-1308

Aerodynamic Phenomena of Retro Propulsion Descent and Landing Configurations

Autores: Marwege, Ansgar; Hantz, Christian; Kirchheck, Daniel; Klevanski, Josef; Vos, Jan; Laureti, Mariasole; Karl, Sebastian; Gulhan,Ali
Publicado en: FAR2022, 2022
Editor: ESA
DOI: 10.5281/zenodo.6783922

Aerothermal analysis of the RETALT2 vehicle

Autores: Mariasole Laureti; Karl, Sebastian
Publicado en: Aerosapce Europe Conference - 10th EUCASS - 9th CEAS, 2023
Editor: 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

Autores: A. Marwege, A. Guelhan, J. Klevanski, J. Riehmer, S. Karl, D. Kirchheck, D. Bonetti, J. Vos, M. Jevons, A. Krammer, J. Carvalho
Publicado en: 70th International Astronautical Congress (IAC), 2019
Editor: 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)

Autores: P. Starke, C. Dorbath, D. Zell
Publicado en: 70th International Astronautical Congress (IAC), 2019
Editor: IAF
DOI: 10.5281/zenodo.5770094

RETALT - RETro propulsion Assisted Landing Technologies

Autores: A. Guelhan, A. Marwege, J. Klevanski, S. Karl, D. Bonetti, J. Vos, M. Jevons, A. Krammer, J. Carvalho
Publicado en: Internation Plenatry Probe Workshop, 2019
Editor: 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)

Autores: P. Starke, C. Dorbath
Publicado en: EUCASS, 2019
Editor: EUCASS
DOI: 10.5281/zenodo.5779163

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

Autores: Thies, Christoph
Publicado en: FAR2022, 2022
Editor: ESA
DOI: 10.5281/zenodo.6759766

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

Autores: De Zaiacomo, G.; Medici, G.; Princi, A.; Ghignoni, P.; Botelho, A.; Martinez Arlandis, M.; Recupero,C.; Fabrizi, A.; Fernandez, F.; Guidotti, G.
Publicado en: IAC 2022 Conference, Edición 1, 2022
Editor: IAC
DOI: 10.5281/zenodo.7064630

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

Autores: Krammer, Anett; Nebuloni, Stefano; Lichtenberger, Marc
Publicado en: FAR2022, 2022
Editor: ESA
DOI: 10.5281/zenodo.6759777

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

Autores: Martinez, Marc; Ghignoni, Pietro; Botelho, Afonso; Recupero, Cristina; Fabrizi, Andrea; Fernandez, Vincente; De Zaiacomo, Gabriele
Publicado en: FAR2022, 2022
Editor: ESA
DOI: 10.5281/zenodo.6759659

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

Autores: Ghignoni, P.; Botelho, A.; Recupero, C.; Fernandez, V.; Fabrizi, A.; De Zaiacomo, G.
Publicado en: HiSST Conference, Edición 1, 2022
Editor: HiSST Organizers
DOI: 10.5281/zenodo.7064613

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

Autores: Botelho, A.; Recupero, C.; Fernandez, V.; Fabrizi, A.; De Zaiacomo, G.
Publicado en: ICATT, 2021
Editor: International Conference on Astrodynamics Tools and Techniques
DOI: 10.5281/zenodo.5779496

TPS Design and Manufacturing for the RETALT VTVL launcher

Autores: João Carvalho, Cládia Peixoto, Marta Reinas, Sofia Paixão
Publicado en: CEAS Space Journal, 2022, ISSN 1868-2510
Editor: Springer
DOI: 10.1007/s12567-021-00417-w

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

Autores: Marwege, Ansgar; Kirchheck, Daniel; Klevanski, Josef; Gulhan, Ali
Publicado en: CEAS Space Journal, 2022, ISSN 1868-2510
Editor: 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

Autores: Thies, Christoph
Publicado en: CEAS Space Journal, Edición 1, 2022, ISSN 1868-2502
Editor: Springer Verlag
DOI: 10.1007/s12567-022-00456-x

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

Autores: Charbonnier, Dominique; Vos, Jan; Marwege, Ansgar; Hantz, Christian
Publicado en: CEAS Space Journal, Edición 2, 2022, ISSN 1868-2510
Editor: Springer
DOI: 10.1007/s12567-022-00431-6

Unsteady Aerodynamics of the Retropropulsion Reentry Burn of Vertically Landing Launchers

Autores: Marwege, A.; Gülhan, A.
Publicado en: AIAA Journal of Spacecraft and Rockets, Edición 4, 2023, ISSN 1533-6794
Editor: AIAA
DOI: 10.2514/1.A35647

Mission Engineering for the RETALT VTVL launcher

Autores: Gabriele De Zaiacomo, Gonzalo Blanco Arnao, Riccardo Bunt, Davide Bonetti
Publicado en: CEAS Space Journal, 2022, ISSN 1868-2510
Editor: Springer
DOI: 10.1007/s12567-021-00415-y

RETALT: review of technologies and overview of design changes

Autores: 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
Publicado en: CEAS Space Journal, 2022, ISSN 1868-2510
Editor: 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)

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

Retro propulsion assisted landing technologies: the RETALT project

Autores: Gülhan, Ali; Marwege, Ansgar; Vos, Jan
Publicado en: CEAS Space Journal, 2022, ISSN 1868-2510
Editor: Springer
DOI: 10.1007/s12567-022-00460-1

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

Autores: Anett Krammer, Marc Lichtenberger, Luc Blecha
Publicado en: CEAS Space Journal, 2022, ISSN 1868-2510
Editor: Springer
DOI: 10.1007/s12567-021-00421-0

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

Autores: Laureti, Mariasole; Karl, Sebastian
Publicado en: CEAS Space Journal, 2022, ISSN 1868-2510
Editor: Springer
DOI: 10.1007/s12567-021-00413-0

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

Autores: Afonso Botelho, Marc Martinez, Cristina Recupero, Andrea Fabrizi, Gabriele De Zaiacomo
Publicado en: CEAS Space Journal, 2022, ISSN 1868-2510
Editor: Springer
DOI: 10.1007/s12567-022-00423-6

Resultado final

Publicaciones

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