Advances in Aerospace Propulsion Engineering

Selected Papers of 2025 1st International Conference on Aerospace Propulsion Engineering (ICAPE)
Erscheinungsjahr 2027
ISBN: 978-981-9246-98-4
Verlag: Springer

Buch, Englisch, 436 Seiten, Format (B × H): 155 mm x 235 mm

Reihe: Springer Aerospace Technology

This book features a selection of peer-reviewed papers presented at the 2025 1st International Conference on Aerospace Propulsion Engineering (ICAPE). Topics of interest focus on rocket propulsion, air-breathing propulsion, hybrid air-breathing and rocket propulsion, aeroelectric propulsion, fuels and propellants, environmental impacts of propulsion, emerging energy sources for propulsion, advanced propulsion concepts and technologies, etc. The goal of this book is to contribute to the advancement of aerospace propulsion engineering and to inspire innovative solutions for the challenges of the future.
It can serve as a valuable resource for professionals in aerospace propulsion fields, including engineers, scholars, researchers, and others, fostering the exchange of experiences, novel ideas, research findings, and discussions on encountered challenges and adopted solutions.

Zielgruppe

Research

Autoren/Hrsg.

Liang, Guozhu

Wang, Zhanxue

Fachgebiete

• Technische Wissenschaften Sonstige Technologien | Angewandte Technik Astronautik
• Technische Wissenschaften Maschinenbau | Werkstoffkunde Maschinenbau Triebwerkstechnik, Energieübertragung
• Technische Wissenschaften Verkehrstechnik | Transportgewerbe Luft- und Raumfahrttechnik, Luftverkehr

Inhaltsverzeichnis

Optimization Design for Expander Cycle Liquid Rocket Engine Systems.- Bifurcation Induced Propellant Budgeting Uncertainty of Spacecraft Reaction Control Systems.- Data-driven Research on Dynamic Spray Characteristics of Bipropellant Injector in Pulse Mode.- Conceptual Design of a Micro-Scale Solid Divert and Attitude Control System.- Experimental Analysis of Contact Seal Leakage in Aircraft Engine Casings.- Flow Investigation in Centrifugal Injector of a Liquid Rocket Engine.- Experimental Investigation on the Ignition of a Low-Cost, Green and Non-Toxic HAN-Based Thruster.- Comparison of the Effects of Slot and Air-Entraining Jet on the Performance of Compressor Cascade.- Application Research of Spring-Energized Seal Rings in Liquid Oxygen/Methane Engine.- Low-cycle Fatigue Life Prediction of Turbine Disks based on the Equalized Timescale Method.- Research on Microwave Propulsion Control Method for Spacecraft Based on Multi-Unit Resonant Cavity.- Finite-element Analysis of Vibration Fatigue Life of Al-Li Alloy Rocket Tank.- Numerical Calculation of the Transient Temperature Field in NEPE Propellant Detonation.- Research on Reliability Assessment and Test Planning Method for Reusable Rocket Engines.- Investigation of Hybrid Rocket Motor Regression Rate Coupled with Gas-Phase Radiation Effects.

Über Autor(innen)

Prof. Liang Guozhu obtained his Ph.D degree from the School of Astronautics at Beihang University (BUAA) in China.  He is currently a professor  and doctoral supervisor at the School of Astronautics, Beihang University. His research focuses on the principles, design, and testing  of  solid and liquid rocket propulsion systems.

Prof.  Wang Zhanxue obtained his Ph.D. degree from the Aircraft Engine Department at Northwestern Polytechnical University (NPU) in China. He is currently a professor and doctoral supervisor at the School of Power and Energy, Northwestern Polytechnical University. His research focuses on the overall performance design and multidisciplinary optimization of aircraft engines, and the aerodynamic design and optimization of new exhaust systems.