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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.
Author: | Ralf StarkORCiD, Sebastian Bartel, Florian Ditsche, Thomas EschORCiD |
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Parent Title (English): | Aerospace Europe Conference 2023 - 10th EUCASS - 9th CEAS |
Document Type: | Conference Proceeding |
Language: | English |
Year of Completion: | 2023 |
Date of the Publication (Server): | 2024/07/23 |
Length: | 9 Seiten |
Note: | Lausanne, July 9-13, 2023 |
Link: | https://elib.dlr.de/196178/ |
Zugriffsart: | weltweit |
Institutes: | FH Aachen / ECSM European Center for Sustainable Mobility |
open_access (DINI-Set): | open_access |