Design study of a 30kN LOX/LCH4 aerospike rocket engine for lunar lander application
- Based on lunar lander concept EL3, various LOX/CH4 aerospike engines were studied. A distinction was made between single and cluster configurations as well as ideal and non-ideal contour concepts. It could be shown that non-ideal aerospike engines promise a significant payload gain.
| Verfasserangaben: | Ralf StarkORCiD, Sebastian Bartel, Florian Ditsche, Thomas EschORCiD |
|---|---|
| Titel des übergeordneten Werkes (Englisch): | Aerospace Europe Conference 2023 - 10th EUCASS - 9th CEAS |
| Dokumentart: | Konferenzveröffentlichung |
| Sprache: | Englisch |
| Erscheinungsjahr: | 2023 |
| Datum der Publikation (Server): | 23.07.2024 |
| Umfang: | 9 Seiten |
| Bemerkung: | Lausanne, July 9-13, 2023 |
| Link: | https://elib.dlr.de/196178/ |
| Zugriffsart: | weltweit |
| Fachbereiche und Einrichtungen: | FH Aachen / ECSM European Center for Sustainable Mobility |
| open_access (DINI-Set): | open_access |
