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  • session IP

    Title

    Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

    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

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    6

    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

    7

    Hybrid propulsion systems for reconfigurable small satellite constellations

    10

    confirmed

    Ms. Chloe Gentgen

    Massachusetts Institute of Technology (MIT)

    United States

    9

    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

    21

    Electromagnetic rocket launch system

    10

    confirmed

    Mr. Heet Naik

    University of Mumbai

    India

    1001

    A Contemporary Approach to Propulsion System for an Interplanetary Mission to Venus

    10

    withdrawn

    Mr. Dhruv Gajjar

    Ramaiah Institute of Technology

    India

    1002

    Technology roadmap models for liquid propulsion system development for Indian Space Programme

    10

    confirmed

    Mr. SHREEJITH TV

    Liquid Propulsion System centre

    India

    1003

    Computational Analysis of Boundary layer in Dual Throat Nozzle with secondary injection.

    10

    confirmed

    Ms. Deeksha K

    R V College of Engineering, Bengaluru

    India

    1004

    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

    1005

    Discharge instability in applied field magnetoplasmadynamic thrusters

    10

    Dr. Jian Li

    National University of Defense Technology

    China

    1008

    IGNITION-DELAY MEASUREMENT FOR DROP TEST WITH GREEN HYPERGOLIC PROPELLANTS

    10

    withdrawn

    Ms. Seonghyeon Park

    Hanbat National University

    Korea, Republic of

    1010

    Large Eddy Simulations for Combustion Dynamics in Liquid Rocket Engines

    10

    confirmed

    Mr. Abhishek Sharma

    Indian Space Research Organization (ISRO)

    India

    1011

    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

    1012

    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

    1013

    Porous Bodies Research for Dynamic Seal Development

    10

    Prof.Dr. Mykhailo Katrenko

    Oles Honchar Dnipropetrovsk National University

    Ukraine

    1014

    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

    1015

    propellant mass flow rate control scheme of a deep-throttling rocket engine

    10

    confirmed

    Mr. Runsheng Hu

    National University of Defense Technology

    China

    1016

    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

    1017

    system analysis of feed system coupled combustion stability in liquid rocket engines

    10

    confirmed

    Dr. meng dong

    Xi'an Aerospace Propulsion Institute

    China

    1018

    Study of Magneto-Plasma Dynamic thruster system

    10

    withdrawn

    Mr. Paras Adlakha

    University of Petroleum and Energy Studies

    India

    1019

    Research on Circuit with Ignition Constant Current Function in Radio frequency Ion Thruster

    10

    confirmed

    Mr. Duan Yonghui

    China Aerospace Corporation

    China

    1020

    Magnetoplasmodynamic electro-jet propulsion device for orbit correction and maneuvers in space

    10

    Mr. Vladimir Shirin

    Kazakhstan