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 |
|---|---|
| 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 |
