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
- Room
- IPC members
Co-Chair: Dr. Vanessa Vial, SAFRAN, France;
Co-Chair: Dr. Mario Kobald, German Aerospace Center (DLR), Germany;
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 |
10 | confirmed | Ms. Charmaine Neufeld | University of British Columbia | Canada | |
10 | confirmed | Mr. Heet Naik | University of Mumbai | India | |
A Contemporary Approach to Propulsion System for an Interplanetary Mission to Venus | 10 | withdrawn | Mr. Dhruv Gajjar | Ramaiah Institute of Technology | 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 |
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 | |
IGNITION-DELAY MEASUREMENT FOR DROP TEST WITH GREEN HYPERGOLIC PROPELLANTS | 10 | withdrawn | Ms. Seonghyeon Park | Hanbat National University | Korea, Republic of |
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 |
10 | confirmed | Mr. ANANT SINGHAL | Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC) | India | |
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 |
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 |
10 | withdrawn | Mr. Paras Adlakha | University of Petroleum and Energy Studies | India | |
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 |