IAF Digital Library

VP

session VP

Title: Virtual 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.

IPC members

Co-Chair: Dr. Elizabeth Jens, Jet Propulsion Laboratory - California Institute of Technology, United States;
Co-Chair: Dr. Vanessa Vial, SAFRAN, France;
Co-Chair: Dr. Yen-Sen Chen, American Institute of Aeronautics and Astronautics (AIAA), United States;
Co-Chair: Dr. Mario Kobald, German Aerospace Center (DLR), Germany;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Design of a gas filled bellow pogo suppression device for launch vehicles.	10	confirmed	Mr. SUNNY MITRA	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
2		Research and application on the innovative design system of LOX Kerosene engine which is available to Additive manufacturing technology	10	confirmed	Mr. WANG Chunmin	Northwestern Polytechnical University，NPU	China
6		A way to increase rocket efficiency: the aerospike engine	10	confirmed	Mr. Baptiste Laulan--Souilhac	ISAE - Institut Supérieur de l'Aéronautique et de l'Espace	France
8		Effect of blade configuration on performance of a high speed axial flow pump inducer	10	confirmed	Mr. AJI M ABRAHAM	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
11		influence of inlet air temperature for dilution mixing in turbine-based air-breathing propulsion system	10	confirmed	Mr. Wei Dai	Beijing institute of Astronautical Systems Engineering, Beijing	China
13		Experimental Studies on the Efficacy of Tabs as Supersonic Jet Control	10	confirmed	Mr. THILLAIKUMAR T	Indian Institute of Technology Kharagpur	India
14		A technology for improving regenerative cooling in advanced cryogenic rocket engines for space transportation	10	confirmed	Mr. AP Baiju	LPSC, ISRO	India
15		Assessment and Design of the Active Air Intake for VLEO Operation	10	confirmed	Mr. Anatolii Papulov	Skolkovo Institute of Science and Technology	Russian Federation
16		MEMS thruster with an alternative ADN based monopropellant	10	confirmed	Mr. Ju Won Kim	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
19		minimum catalyst bed length for high test hydrogen peroxide thrusters	10	confirmed	Mr. Sangwoo Jung	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
22		Design and Test of Non-Uniform Spray Swirl Injectors and Its Applications in Injection Plate Design	10	confirmed	Mr. Alexandre Costa Goulart	Universidade Federal do ABC - UFABC	Brazil
23		Literature studies and experimental characterization of multiple solid propellant regression rates using Crawford bomb method and rocket design analysis	10	confirmed	Mr. Jesús Manuel Muñoz Tejeda	Imperial College London	Spain
24		Prediction of thermoacoustic instabilities by the linearized Navier-Stokes equations incorporated with the nonlinear n-tau model	10	confirmed	Mr. Yuanzhe LIU	Northwestern Polytechnical University	China
25		Fission Fragment Rocket: Fuel Production and Structural Considerations	10	confirmed	Mr. Pauli Laine		Finland
29		Mutation of Permanent Magnet Hall Thruster: Central Cathode Configuration	10	confirmed	Ms. Shritu Badoniya	University of Petroleum and Energy Studies	India
30		Design and Simulation of an Articulated On-board CubeSat Propulsion System	10	confirmed	Ms. Sneha Gayen	SRM Institute of Science and Technology	India