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Akademický článek
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Autor:
Marwege, Rebecca Sophie1 rsm2194@columbia.edu
Publikováno v:
Political Theology. Dec2022, Vol. 23 Issue 8, p768-781. 14p.
Akademický článek
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Autor:
Marwege, Ansgar, Hantz, Christian, Kirchheck, Daniel, Klevanski, Josef, Gülhan, Ali, Charbonnier, Dominique, Vos, Jan
Publikováno v:
CEAS Space Journal
In the RETALT (RETro propulsion Assisted Landing Technologies) project vertical landing launcher configurations are investigated. In the aerodynamic phase of retro propulsion assisted descent and landing, the main devices for control and trim of the
Autor:
Rebecca Sophie Marwege
Publikováno v:
Political Theology. 23:768-781
This article argues that Hobbes’ contradictory references to God can be resolved if viewed through the lens of two prominent conceptualizations of God – the Reformist hidden God (deus absconditus) ...
In the frame of the RETALT (RETro propulsion Assisted Landing Technologies) project, the aerodynamics of reusable launch vehicles reentering the atmosphere and descending and landing with the aid of retro propulsion are studied. In particular, series
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1e3c873d46d390909a77250d5ac62236
https://elib.dlr.de/188153/
https://elib.dlr.de/188153/
In the frame of the RETALT project a large number of CFD simulations and Wind Tunnel experiments were made for both the RETALT1 and RETALT2 configurations to better understand the physics and mechanisms of retro-propulsion at supersonic flow conditio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1d6313f215fbd84b570e906a24bbc3a6
Autor:
Marwege, Ansgar, Hantz, Christian, Kirchheck, Daniel, Klevanski, Josef, Vos, Jan, Laureti, Mariasole, Karl, Sebastian, Gülhan, Ali
The RETALT (RETro propulsion Assisted Landing Technologies) project aims to investigate vertically landing launcher configurations, which decelerate by means of retro propulsion manoeuvres during the descent and final landing phase. One key objective
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::23b925e518cdb41c6aa42f3805ef8547
https://doi.org/10.5281/zenodo.6783922
https://doi.org/10.5281/zenodo.6783922
The RETALT (Retro Propulsion Assisted Landing Technologies) project aims at investigating launch system reusability technologies for two different Vertical Take-off Vertical Landing launcher configurations, namely RETALT1 and RETALT2. This paper desc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::11276d341c31c37ef42003bd4d436387
Autor:
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.
Since SpaceX successfully demonstrated the vertical landing of launcher first stages and made this way of returning them to earth a routine operation with over 100 successful landings after 6 years, the interest in Europe to develop the key technolog
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::211afefed185b8b1fc51ae41bdf3663e