Assenmacher, Oliver and Dabanovic, Andrija and Poppe, Georg and Rüttgers, Alexander (2024) Automatic Outlier Detection for Hybrid Rocket Static Firing Tests. In: Proceedings of the International Astronautical Congress, IAC. International Astronautical Federation, IAF. 75th International Astronautical Congress (IAC), 2024-10-14 - 2024-10-18, Mailand, Italien. ISSN 0074-1795.
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Abstract
A method for automatically detecting anomalous events in the video recordings of a static firing test was developed. It has been evaluated on a test of the VISERION hybrid rocket engine designed at the German Aerospace Center (DLR). Static firing tests are an important step in the design and qualification of rocket engines as they provide a controlled environment for evaluating the safety and performance of a rocket motor. The temperatures and pressures in different parts of the motor as well as the thrust and videos of the exhaust plume can be recorded to gain insight into the characteristics of the propulsion system. However, manual analysis of this data quickly reaches its limits due to the large amount of raw data. Therefore, this manuscript explores an automated approach to extract insights from this data. Specifically, a procedure is developed to automatically detect outliers in video recordings of the exhaust plume based on the Local Outlier Probabilities algorithm. This method is applied to a static firing test of the VISERION hybrid rocket engine. The engine uses a propellant combination of HTPB and hydrogen peroxide and produces a thrust of approximately 11.5 kN over a burn time of 28 s. In a second static firing, an insufficient composite thermal protection component was used, resulting in delaminations and small pressure increases due to nozzle blockage. The influence on the exhaust plume was recorded by cameras from different angles. The automatic procedure clearly identifies the respective outliers, indicating a promising approach for detailed analyses of engine test data.
| Item URL in elib: | https://elib.dlr.de/207630/ | ||||||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||||||
| Title: | Automatic Outlier Detection for Hybrid Rocket Static Firing Tests | ||||||||||||||||||||
| Authors: |
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| Date: | 15 October 2024 | ||||||||||||||||||||
| Journal or Publication Title: | Proceedings of the International Astronautical Congress, IAC | ||||||||||||||||||||
| Refereed publication: | No | ||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||
| Publisher: | International Astronautical Federation, IAF | ||||||||||||||||||||
| ISSN: | 0074-1795 | ||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||
| Keywords: | Hybrid Propulsion, Anomaly Detection, Machine Learning, Computer Vision, Combustion | ||||||||||||||||||||
| Event Title: | 75th International Astronautical Congress (IAC) | ||||||||||||||||||||
| Event Location: | Mailand, Italien | ||||||||||||||||||||
| Event Type: | international Conference | ||||||||||||||||||||
| Event Start Date: | 14 October 2024 | ||||||||||||||||||||
| Event End Date: | 18 October 2024 | ||||||||||||||||||||
| Organizer: | International Astronautical Federation (IAF) | ||||||||||||||||||||
| 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 - Synergy Project Advanced Technologies for High Energetic Atmospheric Flight of Launcher Stages, no assignment | ||||||||||||||||||||
| Location: | Köln-Porz | ||||||||||||||||||||
| Institutes and Institutions: | Institute of Software Technology > High-Performance Computing Institute of Software Technology Responsive Space Cluster Competence Center > Launch Segment Responsive Space Cluster Competence Center Institute for Aerodynamics and Flow Technology > Spacecraft, BS Institute for Aerodynamics and Flow Technology | ||||||||||||||||||||
| Deposited By: | Assenmacher, Oliver | ||||||||||||||||||||
| Deposited On: | 02 Dec 2024 14:40 | ||||||||||||||||||||
| Last Modified: | 11 Jan 2025 19:47 |
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