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: 2022-09-21
Time: 13:30
Room: IP Area

IPC members

Co-Chair: Dr. Elizabeth Jens, Jet Propulsion Laboratory - California Institute of Technology, United States;
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: Dr. Mario Kobald, German Aerospace Center (DLR), Germany;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	PEPE: A low cost, reliable, reusable, user- and environment- friend Propulsion System	10	confirmed	Mr. Luciano Battocchio		Czech Republic
2	Optimized orbit transfer of a Gravidyne with low-thrust propulsion	10	confirmed	Mr. David Gil	United Arab Emirates University (UAEU)	United Arab Emirates
3	Experimental Investigation on Throttling Transient Response of Bipropellant Thruster Using Cavitating Venturi Valve.	10	confirmed	Mr. Vincent Ugolini	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
4	The Turborocket Engine: An Integrated Pump-Fed Rocket Engine for Propulsion Applications	10	withdrawn	Dr. John Bossard		United States
5	Physical properties and ignition characteristics of hypergolic propellant with oxidizing additives	10	confirmed	Mr. Kyounghwan Lee	Hanbat National University	Korea, Republic of
6	ignition delay and thermoacoustic coupling in hybrid rocket combustion	10	confirmed	Prof. Changjin Lee	Konkuk University	Korea, Republic of
7	two-phase, multicomponent hydrogen peroxide blowdown injector modelling and tests comparisons	10	confirmed	Mr. Arthur Bahdur	Alcântara Launch Center	Brazil
8	Wave Steepening Instability Caused by Hypergolic Detonation of High Test Peroxide-based Hypergol	10	withdrawn	Mr. Kyu-Seop Kim	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
9	Numerical and experimental investigation of lambda type seals in high-pressure cryogenic bolted joints	10	confirmed	Mr. B Deependran	Indian Space Research Organization (ISRO)	India
10	Designing a nuclear electric propulsion system for future Pluto missions	10	confirmed	Mr. Maanyash Jain		India
11	ST-40 Hall Thruster Testing with LaB6 Hollow Cathode	10		Prof. Olexandr Petrenko	Flight Control LLC	Ukraine
12	Strategy for Simultaneous Hydrogen Trapping and Metallic Grain Size Control in Cermet Fuels for Nuclear Thermal Propulsion	10	confirmed	Mr. Jonathan Johnson	The University of Alabama	United States
13	Conceptual Design of a N2O/Paraffin Hybrid Sounding Rocket	10	confirmed	Mr. Riccardo Gelain	Université Libre de Bruxelles	Belgium
14	Parametric design and testing of explosion-preventive solid propellant rocket engines in the event of unexpected behavior during combustion	10	confirmed	Mr. Nicolás de Jong	LEEM-UPM	Spain
15	Nuclear Thermal Propulsion for In-Space Applications focusing Beryllium as the Working Fluid and Graphite and FLiBe as Moderator and Coolant and Thorium Blanket	10	confirmed	Ms. Aarya Kulkarni	International Space University (ISU)	India
16	Propellant grain design for Solid strap-on Booster operating under Martian condition and selecting the appropriate propellant.	10	confirmed	Mr. Mahir Rawal		India
17	The Relativistic Mass Ratio in Ultrarelativistic Photon Rockets	10		Prof. Espen Haug	Norwegian University of Science and Technology	Norway
18	Simulation analysis of multimode propulsion systems for satellites	10	withdrawn	Ms. Sagarika Rao Valluri	RNSIT Bangalore	India
19	Pulsed Plasma Thruster for Deep Space Exploration	10	confirmed	Dr. Jayakumar Venkatesan	Valles Marineris International Private Limited	India
20	Electrodeless plasma thruster concepts for high-power propulsion systems	10	confirmed	Dr. Sean Shan Min Swei	Khalifa University of Science and Technology (KUST)	United Arab Emirates
21	Aerodynamic analysis on JAXA’s experimental vehicle for hypersonic flight	10		Dr. Susumu Hasegawa	Japan Aerospace Exploration Agency (JAXA)	Japan
22	Dynamic Modeling and Simulation of a Hydrogen Peroxide Monopropellant Thruster	10	confirmed	Dr. Sukmin Choi	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
23	Three-Dimensional MHD Analysis of Magnetic Plasma Drag with Coils Placed on Three Axes	10	confirmed	Dr. Shoko Arita	Shizuoka University	Japan
24	Conditions for the long-term existence of spacecraft with air-breathing electric propulsion in ultra-low orbits about planets	10	confirmed	Dr. Egor Loktionov	Bauman Moscow State Technical University	Russian Federation
25	A Novel Design Usage of Thermoelectric Materials in Aerospike Engines	10	confirmed	Mr. Gautam Arora	University of Petroleum and Energy Studies	India
26	A Comparison Study on the Feasibility of Two Low Sloshing Configurations for Small Satellite Magnetic Fluid Actuation	10	confirmed	Mr. Priyank Dubey	Indian Institute of Technology	India
27	The nano-probe by the photon transportation in the Deep Space	10	confirmed	Mr. Jamel Metmati	THALES Services	France
28	9tonf staged combustion cycle liquid rocket engine startup analysis	10	confirmed	Mrs. BOYEON KHIM		Korea, Republic of
29	Hypergolic ignition characterization of less-toxic bipropellants using Hydrocarbon fuel blend and Hydrogen Peroxide	10	confirmed	Mr. Vignesh G	ISRO Propulsion Complex, Mahendragiri, India	India
30	Development Status of the SPS-40 Propulsion System	10	confirmed	Mr. Danylo Shcherbak	Flight Control LLC	Ukraine
31	HYDROGEN-ENRICHED LIQUID METHANE AND LIQUID ETHANOL AS A TRANSITIONAL SOLUTION TOWARDS SUSTAINABILITY IN TERMS OF TECHNICAL FEASIBILITY FOR AEROSPACE MISSIONS	10	confirmed	Mr. ILYES GHEDJATTI	Beijing University of Aeronautics and Astronautics (BUAA)	China
32	cold-gas experiments on advanced nozzles in subsonic counter-flows	10	withdrawn	Mr. Giuseppe Scarlatella	Technische Universität Dresden (DTU)	Germany
33	Development of Ultra High DN Ceramic Ball Bearing for Cryogenic Rocket Engine Turbopump	10	confirmed	Mr. BEN JACOB	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
34	The effect of aerodynamic heating to cryogenic propellant discharge	10	confirmed	Dr. Seungwhan Baek	Korea Aerospace Research Institute (KARI)	Korea, Republic of
35	preliminary screening of catalytic beds for hydrogen peroxide thrusters with thrust level lower than 0.5 N	10	confirmed	Mr. Rawoof Shaik	University of Pisa	Italy
36	Numerical Simulation of Flow Atomization caused by Two Impinging Liquid Jets	10	confirmed	Ms. Maryam Ozair	Pakistan Space and Upper Atmosphere Research Commission (SUPARCO)	Pakistan
37	Rapid Design of a Small Scale KeroLOx Flight Vehicle Propulsion System	10	confirmed	Mr. Nathan Hirsch	Viterbi School of Engineering, USC	United States
38	FEASIBILITY ANALYSIS FOR ELECTRIC PROPULSION SYSTEMS FOR SHORT TERM INTERPLANETARY MISSIONS	10	confirmed	Ms. Pritha Pal	University of Michigan	United States
39	Design and development of Latching Solenoid valve for Active Pressure Regulation System	10	confirmed	Mr. Venkata Sunil Sai Nukala	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
40	Computational model for performance prediction of a nitrous oxide / eicosane hybrid rocket engine	10	confirmed	Mr. Joel Jean-Philyppe	McGill University	Canada
41	Common pitfalls of testing hybrid rocket engines at student led facilities	10	confirmed	Mr. Cyril Mani	McGill University	Canada
42	Vacuum Arc Thruster architecture for green orbit maintenance with small satellite missions	10	confirmed	Mr. José-María Jiménez-Coronado	Costa Rica Institute of Technology (ITCR)	Costa Rica
43	Experimental & Numerical Investigation of GOx/GCH4 Combustion in a 7-Element Rocket Combustor	10		Mr. Abhishek Sharma	Indian Space Research Organization (ISRO)	India
44	Numerical study on n-decane heat transfer under supercritical pressure in regenerative cooling channel	10	confirmed	Mr. Yuhang Li	Xi'an Aerospace Propulsion Institute	China
45	Integrated internal and external ballistics for sounding rocket design	10	confirmed	Dr. Jeongmoo Huh	United Arab Emirates University (UAEU)	United Arab Emirates
46	Numerical estimation of heat loss and thrust performance characteristics in micro propulsion	10	confirmed	Dr. Jeongmoo Huh	United Arab Emirates University (UAEU)	United Arab Emirates
47	Comparative analysis of numerical models of film and regenerative cooling in thrust chamber at high pressure	10	confirmed	Mr. Dhiyaneshwar L V	SASTRA University	India
48	multi-scale numerical study on atomization dynamics of gas-liquid pintle injector	10	confirmed	Mr. Pu Shi	Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory, Northwestern Polytechnical University	China
49	Modeling of wall-bounded high pressure flows in Liquid Rocket Engines	10		Mr. Giuseppe Indelicato	Sapienza University of Rome	Italy
50	High Flux Hybrid Motor Development with Distributed Tube Injector	10	confirmed	Mr. Mehmet Kahraman	Deltav Space Technologies,Inc.	Türkiye
51	Research on Acoustic Closed-End Device for Hydraulic Excitation Test of LRE	10	confirmed	Dr. meng dong	Xi'an Aerospace Propulsion Institute	China
52	RESEARCH ON ELECTRIC SPACE PROPULSION AT ITALIAN AEROSPACE RESEARCH CENTRE: status and future enhancement	10	confirmed	Dr. Marco Invigorito	CIRA Italian Aerospace Research Centre	Italy
53	Effect of H2O2 concentration and catalytic ratio on the autoignition characteristics of RP-3 kerosene under catalytic ignition engine-like conditions	10	confirmed	Mr. Shutao Han	Beihang University (BUAA)	China
54	A Review: On the various FEEP thrusters present in the Industry and their Performance Comparison	10	confirmed	Mr. Anirudh Balaji N S	SASTRA University	India
55	Vacuum testing of 3D printed 1N Hydrogen Peroxide thruster and a novel platinum catalyst	10	confirmed	Mr. Varun Reddy Nandyala	FOTEC Forschungs- und Technologietransfer GmbH	Austria
56	Lessons learned during SRAD hybrid rocket motor development	10	confirmed	Mr. Norbert Szulc	Gdansk University of Technology	Poland
57	Using differential pressure sensor to measure nitrous oxide level in a tank	10	confirmed	Mr. Mateusz Czapski	Gdansk University of Technology	Poland

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