TY - GEN
T1 - LSTM-Based Post-Mission Assessment of Reusable Rocket Engines
AU - Li, Tianwen
AU - Zhao, Zeng
AU - Zhang, Yang
AU - Yu, Nanjia
N1 - Publisher Copyright:
Copyright ©2025 by the International Astronautical Federation (IAF). All rights reserved.
PY - 2025
Y1 - 2025
N2 - Reusable rocket technology is having a significant impact on the economics of spaceflight, with the condition of the engine being a fundamental factor in determining its reusability.This study proposes a novel fault diagnosis framework for the evaluation of reusable rocket engines post-mission, with the aim of determining their suitability for continued operational use or the necessity for maintenance.The study utilises deep learning, specifically Long Short-Term Memory (LSTM) networks, to analyse time-series data, including vibration signals, thermodynamic parameters and operational history. This analysis captures temporal patterns that are crucial for assessing the health of the engine. This approach facilitates precise identification of degradation and failure modes that are critical to the decision-making process concerning reuse. The present methodology is centred on the "Reusability Readiness Index" (RRI), a metric that quantifies engine condition by integrating fatigue damage, thermal stress accumulation, and operational anomalies detected via LSTM's sequential data processing.The present framework was validated using post-mission data from ground tests and simulated flight profiles of a liquid rocket engine. The results obtained from this study indicate that the LSTM-based method achieves a classification accuracy of over 90% in determining the reusability or repair requirements of engines, thereby reducing false positives by approximately 15% in comparison with traditional threshold-based approaches. This enhanced precision facilitates reliable post-mission evaluations, optimises maintenance schedules, and streamlines reuse planning. At present, the framework is tailored for post-mission analysis; however, it provides a robust foundation for retrospective engine assessment, offering actionable insights into component wear and performance trends. However, the potential of this framework extends beyond the scope of this study.Future work will build upon this LSTM-based architecture to enable real-time fault monitoring during missions.The incorporation of live sensor feeds, such as pressure transients and thermal fluctuations, and the refinement of the model's computational efficiency, will facilitate a transition from post-flight diagnostics to in-flight health tracking.This evolution will enhance mission safety and operational flexibility, allowing for proactive responses to emerging issues. The adaptation of the framework to diverse engine types will be a key focus area to ensure broader applicability. This research underscores the potential of deep learning in evaluating reusable rocket engines, thereby integrating post-mission analysis with the promise of real-time capabilities.By refining reuse assessments and establishing the foundations for continuous monitoring, our work contributes to the advancement of the reliability and sustainability of reusable spaceflight systems.
AB - Reusable rocket technology is having a significant impact on the economics of spaceflight, with the condition of the engine being a fundamental factor in determining its reusability.This study proposes a novel fault diagnosis framework for the evaluation of reusable rocket engines post-mission, with the aim of determining their suitability for continued operational use or the necessity for maintenance.The study utilises deep learning, specifically Long Short-Term Memory (LSTM) networks, to analyse time-series data, including vibration signals, thermodynamic parameters and operational history. This analysis captures temporal patterns that are crucial for assessing the health of the engine. This approach facilitates precise identification of degradation and failure modes that are critical to the decision-making process concerning reuse. The present methodology is centred on the "Reusability Readiness Index" (RRI), a metric that quantifies engine condition by integrating fatigue damage, thermal stress accumulation, and operational anomalies detected via LSTM's sequential data processing.The present framework was validated using post-mission data from ground tests and simulated flight profiles of a liquid rocket engine. The results obtained from this study indicate that the LSTM-based method achieves a classification accuracy of over 90% in determining the reusability or repair requirements of engines, thereby reducing false positives by approximately 15% in comparison with traditional threshold-based approaches. This enhanced precision facilitates reliable post-mission evaluations, optimises maintenance schedules, and streamlines reuse planning. At present, the framework is tailored for post-mission analysis; however, it provides a robust foundation for retrospective engine assessment, offering actionable insights into component wear and performance trends. However, the potential of this framework extends beyond the scope of this study.Future work will build upon this LSTM-based architecture to enable real-time fault monitoring during missions.The incorporation of live sensor feeds, such as pressure transients and thermal fluctuations, and the refinement of the model's computational efficiency, will facilitate a transition from post-flight diagnostics to in-flight health tracking.This evolution will enhance mission safety and operational flexibility, allowing for proactive responses to emerging issues. The adaptation of the framework to diverse engine types will be a key focus area to ensure broader applicability. This research underscores the potential of deep learning in evaluating reusable rocket engines, thereby integrating post-mission analysis with the promise of real-time capabilities.By refining reuse assessments and establishing the foundations for continuous monitoring, our work contributes to the advancement of the reliability and sustainability of reusable spaceflight systems.
KW - Engine Evaluation
KW - Fault Diagnosis
KW - LSTM
KW - Reusability Readiness Index
KW - Reusable Rockets
KW - Time-Series Analysis
UR - https://www.scopus.com/pages/publications/105036204472
U2 - 10.52202/083090-0094
DO - 10.52202/083090-0094
M3 - 会议稿件
AN - SCOPUS:105036204472
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 877
EP - 886
BT - IAF Space Propulsion Symposium - Held at the 76th International Astronautical Congress, IAC 2025
PB - International Astronautical Federation, IAF
T2 - 2025 IAF Space Propulsion Symposium at the 76th International Astronautical Congress, IAC 2025
Y2 - 29 September 2025 through 3 October 2025
ER -