IPB

session IPB

Title: Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM
type: interactive

IPC members

Co-Chair: Dr. Saroj Kumar, Propulsion Research Center, University of Alabama in Huntsville, United States;
Co-Chair: Dr. Andrei Shumeiko, Bauman Moscow State Technical University, Russian Federation;
Co-Chair: Dr. Elizabeth Jens, Jet Propulsion Laboratory - California Institute of Technology, United States;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
Control Strategies for Storage Enhanced Atmosphere Breathing Electric Propulsion	15		Mr. Cameron Leslie	Cranfield University	United Kingdom
Experimental Validation of Numerical Methodologies in Liquid-Liquid Coaxial Swirl Injector Design	12	confirmed	Mr. Felix Liu	University of Southern California	United States
Sustainable hybrid propulsion: a green approach for future space missions	12	withdrawn	Mr. Osmar Naim Corona Zamudio	High Technology Unit (UAT) Faculty of Engineering - UNAM	Mexico
SuperMagdrive: Next generation propulsion for larger spacecraft	12	confirmed	Mr. Alex Chandler	Magdrive Ltd	United Kingdom
Enhancement of the main sub-systems in Student Researched and Developed (SRAD) Hybrid Rocket Engine (HRE)	13	confirmed	Ms. Małgorzata Majda	Gdansk University of Technology	Poland
Pressurization Analysis of Cryogenic Propellant Tanks: Investigating Collapse Factor and L/D Ratio Influence	10		Mr. Tegin Berkay Budak	ROKETSAN Roket Sanayi ve Ticaret A.S.	Türkiye
Electrohydrodynamic Plasma Generators for Enhanced Electrospray Thruster Performance	15	confirmed	Mr. Joel Eldo	Technical University of Munich	Germany
A Novel Versatile Test Bench for Liquid Bipropellant Rocket Testing and Numerical Combustion Simulations	12	confirmed	Dr. Stefano Mungiguerra	Università degli Studi di Napoli “Federico II”	Italy
Efficient Mission Analysis for Small Satellites: Maneuver Planning, Constellation Deployment, and Propulsion Optimization	12	confirmed	Dr. Giuseppe Di Pasquale	IENAI SPACE	Spain
sustainable propulsion in low earth orbit: algae and seaweed based biofuels for space exploration applications	12	confirmed	Ms. Anchal Bhupal	VIT Bhopal University	India
Designing Advanced Solid and Hybrid Propulsion Systems for Rapid Space Missions: Propellant Enhancements and Thrust Control Innovations	13		Mr. Yuvraj Pagare	University of Hertfordshire	United Kingdom
Integral and probe characteristics of a laboratory model of an accelerator with closed electron drift on a mixture of reactive gases	12	confirmed	Ms. Anastasia Mekh	Bauman Moscow State Technical University	Russian Federation
From Concept to Results: Insights from the HYPROB Demonstrators Line on Methane-based Propulsion	12	confirmed	Dr. Daniele Ricci	CIRA Italian Aerospace Research Center, Capua	Italy
Reduced-order Models for Radiative Heat Loads Estimation in Liquid Rocket Engines	12	confirmed	Mr. Marco Fabiani	Sapienza University of Rome	Italy
Solid Hydrocarbon Propellants for Electrothermal Plasma Micro-Thrusters	15	confirmed	Mr. Thimthana Lee	Australian National University (ANU)	Australia
Time variant nozzle flow efficiency factor for accurate estimation of solid rocket motor thrust	13		Mr. KIRAN PINUMALLA	Vikram Sarabhai Space Centre, Thiruvananthapuram-695 022, INDIA	India
design and testing of a variable thrust hydrogen peroxide/kerosene propulsion system pressurized by electric pumps	10	confirmed	Mr. Xuesong Guo	School of Astronautics, Beihang University	China
Design and Analysis of a Variable Exit Area Nozzle for an Experimental Rocket	13		Mr. Renato Sebastian Gomez Olazo	Universidad Peruana de Ciencias Aplicadas	Peru
Solid Ramjet Gas Generator Fuel: Additive Effects and Altitude Performance Analysis	12		Mr. Abdul Rahman	Scuola di Ingegneria Aerospaziale "La Sapienza"	Italy
Low-order modeling and analysis of propulsion control strategies for autogenous pressurization in methane-oxygen rocket engines	10	confirmed	Mr. Sinyoung Park	Hanbat National University	Korea, Republic of
Development of turbopumps for LE-9, first stage engine of H3 Launch Vehicle	12	confirmed	Mr. Taiichi Motomura		Japan
Critical Assessment of Open and Closed-end Swirl Injector Dynamics for LOx-Methane Rocket Engine Applications	12	confirmed	Dr. Abhishek Sharma	Indian Space Research Organization (ISRO)	India
A review on characteristic of Scramjet Combustor based on fuel selection	12	confirmed	Ms. Srishti Bansal	Space Generation Advisory Council (SGAC)	India
Polymer free coaxial pulsed plasma thruster design and validation	12		Dr. Kostadinos Tsoutas	The University of Sydney	Australia
Testing Campaign of the Solar Electric Propulsion System for the Emirates Mission to the Asteroid Belt	12		Mrs. Mariam Alhammadi	Technology Innovation Institute (TII)	United Arab Emirates
geometrical structure design and optimization on an air-augmented solid rocket combustor	12	confirmed	Mr. Zhaoyang Tian	Northwestern Polytechnical University	China
Validation of Computationally Efficient CFD Models for Flow Field Analysis in Hypersonic Engines	12	confirmed	Mr. Kei Fukuzawa	Kanazawa Institute of Technology	Japan
Aerodynamic Configuration Design and Simulation Analysis of Baffle-Type Fairings	12	confirmed	Dr. Hua Zhang		China
Water-Based Integrated Multimodal Propulsion: A Disruptive Solution for Efficient In-Orbit Servicing and Space Debris Removal Missions	12	confirmed	Dr. Chengyu Ma	Chinese Academy of Sciences	China

session IPB

Paper title

Mode

Presentation status

Speaker

Affiliation

Country