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In the last decade, the number of space-based applications increased dramatically. To cover such a demanding market, launch technologies adapted and new launch solutions were developed, to increase the efficiency and the cost effectiveness of the acc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::35f65c8464f3c5b912272debc7ef575e
Autor:
Martinez, Marc, Ghignoni, Pietro, Botelho, Afonso, Recupero, Cristina, Fabrizi, Andrea, Fernandez, Vincente, De Zaiacomo, Gabriele
This paper presents the GNC concept solution developed for the recovery and landing of Vertical Take-off Vertical Landing (VTVL) launch vehicles in the context of RETALT (RETro-propulsion Assisted Landing Technologies), a European Union Horizon 2020
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::99df8c829fb0789d8b6866c7744ae30c
Autor:
Sciarra, Marcello, de Zaiacomo, Gabriele, Letterio, Federico, Vicario de Miguel, G., Molinari, Giulio, Aranda Rosales, M., Willems, Sebastian, Van den Eynde, Jeroen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1640::a4e4dfeebff2d04a78f834d439c55408
https://elib.dlr.de/190870/
https://elib.dlr.de/190870/
Autor:
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
Publikováno v:
CEAS space journal. 14(3)
RETALT (RETro propulsion Assisted Landing Technologies) is a project funded in the frame of the European Union Horizon 2020 program, that is studying critical key technologies for the vertical landing of launcher configurations with the aid of retro
Publikováno v:
CEAS Space Journal
In the last decade, the rapid and successful development of reusable launch systems such as SpaceX’ Falcon 9 demonstrated both the operational feasibility of reusable launchers and their economic viability. The objective of recovering a launcher or
Autor:
Alforja Ruiz, Iñigo, Ayala Fernández, Lucía, De Oliveira, Alice, Dominguez Calabuig, Guillermo, Guadagnini, Jacopo, Lantelme, Melissa, Bartoli, Nathalie, Chedevergne, François, De Zaiacomo, Gabriele, Dubreuil, Sylvain, Lavagna, Michèle, Prevereaud, Ysolde, Stoll, Enrico
Publikováno v:
IAC 2021-72nd International Astronautical Congress
IAC 2021-72nd International Astronautical Congress, Oct 2021, Dubaï, United Arab Emirates. pp.IAC-21-D2.4.6
IAC 2021-72nd International Astronautical Congress, Oct 2021, Dubaï, United Arab Emirates. pp.IAC-21-D2.4.6
International audience; Reusable Launch Vehicles (RLVs) are not only key for an economically and ecologically sustainable space access but also represent a paramount innovation towards the increasing demand for smaller satellites and megaconstellatio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::583063ff7a97b22c99d6addd6f071060
https://hal.science/hal-03436658/document
https://hal.science/hal-03436658/document
Design of the landing guidance for the retro-propulsive vertical landing of a reusable rocket stage.
Publikováno v:
CEAS Space Journal; Jul2022, Vol. 14 Issue 3, p551-564, 14p
Autor:
Deimos Space S.R.L., Bucharest, Romania, Medici Giovanni, Ionita Alina, Yabar Valles Celia, DE Zaiacomo Gabriele, Kerr Murray, Pina Caballero Fernando, Russo Antonio, Esa-Estec, Noordwijk, Netherlands, Deimos Space S.L.U., Tres Cantos, Spain, Recupero Cristina
Publikováno v:
INCAS Bulletin, Vol 10, Iss 2, Pp 75-90 (2018)
The ESA REVLANSYS study aims to develop key technologies in the field of Mission Engineering and GNC for autonomous re-entry vehicles, and to derive coherent mission, system and GNC requirements for the specific terminal entry and landing phases. As
Autor:
BONETTI, Davide, DE ZAIACOMO, Gabriele, ARNAO, Gonzalo Blanco, MEDICI, Giovanni, FUENTES, Irene Pontijas, PARREIRA, Baltazar
The ESA Space Rider program aims at providing Europe with an affordable, independent, reusable end-to-end integrated space transportation system, for routine access and return from low orbit. It will be used to transport payloads for an array of appl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e1733712d4d21163fa8959ad1b21d302