IAF Digital Library

IP

session IP

Title: Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM
type: interactive
Description: Authors with an abstract accepted for an interactive presentation will be asked to prepare slides and display them for the duration of the congress on plasma screens. Authors will be assigned to interactive sessions in which they must be near the plasma screens to engage in interactive discussions with other congress attendees.

IPC members

Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;
Co-Chair: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;
Co-Chair: Prof. Riheng Zheng, Beihang University, China;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
ROLE OF ACOUSTICS ON UNSTABLE FIRE PHENOMENON IN SPACE PROPULSION	10	confirmed	Mr. Vinayak Malhotra	SRM University Chennai	India
Research on the acoustic characteristics of flow distribution plate in LOX/kerosene staged combustion rocket engine	10	confirmed	Dr. chen cao	Xian Aerospace Propulsion Institute	China
Review on the technology of liquid oxygen kerosene engine for the booster stage of Long March 5	10	confirmed	Prof. Chen Jianhua	Xi'an Aerospace Propulsion Institute	China
Fusion-Enabled Plasma Propulsion for Enabling Interstellar Missions	10		Mr. ravinder singh	Concordia University	Canada
Fabrication and propulsion performance testing of a 100 mN class resistojet thruster	10	confirmed	Mr. Mohamed Elawad	United Arab Emirates University (UAEU)	United Arab Emirates
Sidewall-mounted planar type propulsion system for post mission disposal of Cubesats	10	confirmed	Dr. Daeban Seo	Korea Aerospace Research Institute (KARI)	Korea, Republic of
Magnetic Octupole Plasma Thruster with a Center-Mounted Hollow Cathode	10	confirmed	Mr. Jordan Hsieh	National Cheng Kung University	Taiwan, China
Direct thrust measurements of multidirectional plasma thruster operated in Krypton	10	confirmed	Mr. Andrei Shumeiko	Bauman Moscow State Technical University	Russian Federation
Advanced Room Temperature Propellants for Rockets and Spacecrafts	10	confirmed	Mr. Ansh Jaipuria	SRM Institute of Science and Technology	India
Energetic and Sustainable Rocket Propellant for Lower Stage	10	confirmed	Mr. BHUSHAN THOMABRE	SRM Institute of Science and Technology	India
experimental study on oxygenation constant volume combustion characteristics of hydrogen internal combustion engine	10	confirmed	Dr. Liqiang Ai	China Academy of Launch Vehicle Technology (CALT)	China
Magnetically Levitated Test Stand for Thrust Measurement for Micro Propulsion Systems	10	confirmed	Mr. Basel Altawil	Khalifa University of Science and Technology (KUST)	United Arab Emirates
THE EFFECT OF SWIRL INJECTION PARAMETERS ON A VORTEX-COOLED THRUSTER FABRICATED USING THERMOPLASTICS AND METAL	10	confirmed	Mr. Mousa Aqailan	United Arab Emirates University (UAEU)	United Arab Emirates
renewable liquid propellants: decarbonizing space exploration	10	confirmed	Prof.Dr. Nazim Muradov	University of Central Florida (UCF)	United States
Research Progress and Future Prospects of Novel Liquid Propellant	10	confirmed	Mr. Xing Zhang	China Aerospace of Science and Technology Corporation	China
Development of Atlas: A Liquid Rocket Engine Cryogenic Test Stand and Feed System	10	confirmed	Mr. Johannes Reichert	Viterbi School of Engineering, USC	United States
Computational simulation of boron oxidation by atmospheric air oxygen using Reactive Molecular Dynamics	10	confirmed	Prof.Dr. José Rocco	ITA-DCTA	Brazil