session LBA

Design and Experimental Validation of a Mass-Efficient Pancake Hybrid Rocket Motor with Vortex-Induced Flow for In-Space Application

confirmed

Ms. Beste Boybasi

Koc University

Türkiye

Effects of seeded hydrogen on zirconium alloys for thermal propulsion

Dr. Phylis Makurunje

Bangor University

United Kingdom

Enhancing Ignition Performance and Self-Sustained Combustion via Wire Vibration in a Water–Metal Micropropulsion System

confirmed

Mr. Minwoo Han

The University of TOKYO, Graduate school

Japan

Ground Testing of High-Thrust Semi-Cryogenic Engine in ISRO: Mechanical Design Challenges and solutions

confirmed

Mr. Vivek S

Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)

India

Hybrid Rocket Development with Nytrox Blends Through Real-Gas Modeling and Planned Hot-Fire Testing for In-Space Applications

confirmed

Mr. Mehmet Kemal Ergin

Koc University

Türkiye

Waste-to-Thrust: Assessing the Viability of Recycled Refuse as Sustainable Propellant for Hybrid and In-Space Propulsion Systems

confirmed

Mr. Ibukunoluwa Afolabi

Space Generation Advisory Council (SGAC)

Nigeria

early-warning method for flame blowout in strut/cavity combined flameholders based on photoelectric-signal

confirmed

Mr. Boyang Chi

College of Astronautics, Northwestern Polytechnical University

China

experimental investigation of combustion characteristics and radical predictions in a strut-cavity combustor

confirmed

Mr. Yi Gao

Northwestern Polytechnical University

China

Study on the combustion characteristics of LOX/kerosene pintle injector based on the state of liquid oxygen

confirmed

Mr. Yaming Zhao

School of Astronautics, Beihang University

China

Study on the Influence of Different Methane Injection Strategies on the Combustion Characteristics of RBCC Engines

Mr. Hui Liu

Northwestern Polytechnical University

China