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.
Date: 2021-10-28
Time: 13:15
Room: IP Area

IPC members

Co-Chair: Dr. Vanessa Vial, SAFRAN, France;
Co-Chair: Dr. Mario Kobald, German Aerospace Center (DLR), Germany;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
Finite element method based failure prediction and redesign of a launch vehicle valve	10	confirmed	Mr. Sarath Chandran Nair S	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
Hybrid propulsion systems for reconfigurable small satellite constellations	10	confirmed	Ms. Chloe Gentgen	Massachusetts Institute of Technology (MIT)	United States
Investigation of Numerical Modeling Methods for Liquid Fuel Combustion and Applications for Small-Scale Bipropellant Liquid Rocket Engines	10	confirmed	Ms. Charmaine Neufeld	University of British Columbia	Canada
Electromagnetic rocket launch system	10	confirmed	Mr. Heet Naik	University of Mumbai	India
Technology roadmap models for liquid propulsion system development for Indian Space Programme	10	confirmed	Mr. SHREEJITH TV	Liquid Propulsion System centre	India
Computational Analysis of Boundary layer in Dual Throat Nozzle with secondary injection.	10	confirmed	Ms. Deeksha K	R V College of Engineering, Bengaluru	India
conceptual design of a small satellite propulsion system for enhanced attitude and orbit control capabilities using multimode propulsion technique	10		Ms. Kanchan Bhale	Space Generation Advisory Council (SGAC)	India
Discharge instability in applied field magnetoplasmadynamic thrusters	10		Dr. Jian Li	National University of Defense Technology	China
Large Eddy Simulations for Combustion Dynamics in Liquid Rocket Engines	10	confirmed	Mr. Abhishek Sharma	Indian Space Research Organization (ISRO)	India
Modeling and Numerical Analysis for Separation Flow and Side-loads in Liquid Rocket Engine Nozzle	10	confirmed	Dr. Ziliang Li	Beijing Aerospace Propulsion Institute	China
Numerical Simulation of High Temperature Gas Condensation in a Flowing Cryogenic Liquid in Semicryogenic engine	10	confirmed	Mr. ANANT SINGHAL	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
Porous Bodies Research for Dynamic Seal Development	10		Prof.Dr. Mykhailo Katrenko	Oles Honchar Dnipropetrovsk National University	Ukraine
Prediction on the reuse number of liquid rocket engine by developing a generalized life model	10	confirmed	Mr. Shijie Liu	Beijing Aerospace Propulsion Institute	China
propellant mass flow rate control scheme of a deep-throttling rocket engine	10	confirmed	Mr. Runsheng Hu	National University of Defense Technology	China
research on the suppression methods of high frequency pressure pulsation in combustion chamber for liquid rocket engine	10	confirmed	Dr. chen cao	Xian Aerospace Propulsion Institute	China
system analysis of feed system coupled combustion stability in liquid rocket engines	10	confirmed	Dr. meng dong	Xi'an Aerospace Propulsion Institute	China
Research on Circuit with Ignition Constant Current Function in Radio frequency Ion Thruster	10	confirmed	Mr. Duan Yonghui	China Aerospace Corporation	China
Magnetoplasmodynamic electro-jet propulsion device for orbit correction and maneuvers in space	10		Mr. Vladimir Shirin		Kazakhstan

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