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Einicke, Karina (2021) Mixture Ratio and Combustion Chamber Pressure Control of an Expander-Bleed Rocket Engine with Reinforcement Learning. Diploma, TU Dresden.
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| Item URL in elib: | https://elib.dlr.de/142247/ | ||||||||
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| Document Type: | Thesis (Diploma) | ||||||||
| Title: | Mixture Ratio and Combustion Chamber Pressure Control of an Expander-Bleed Rocket Engine with Reinforcement Learning | ||||||||
| Authors: |
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| Date: | 2021 | ||||||||
| Refereed publication: | No | ||||||||
| Open Access: | Yes | ||||||||
| Number of Pages: | 83 | ||||||||
| Status: | Published | ||||||||
| Keywords: | liquid rocket engine control, reinforcement learning, reusable rocket engine | ||||||||
| Institution: | TU Dresden | ||||||||
| Department: | Fakultät Maschinenwesen | ||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||
| HGF - Program: | Space | ||||||||
| HGF - Program Themes: | Space Transportation | ||||||||
| DLR - Research area: | Raumfahrt | ||||||||
| DLR - Program: | R RP - Space Transportation | ||||||||
| DLR - Research theme (Project): | R - Project LUMEN (Liquid Upper Stage Demonstrator Engine) | ||||||||
| Location: | Lampoldshausen | ||||||||
| Institutes and Institutions: | Institute of Space Propulsion > Rocket Engine Systems | ||||||||
| Deposited By: | Hanke, Michaela | ||||||||
| Deposited On: | 12 May 2021 07:00 | ||||||||
| Last Modified: | 12 May 2021 07:00 |
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