session IP
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
2022-09-21
- Time
- Room
- 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;
Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
---|---|---|---|---|---|
PEPE: A low cost, reliable, reusable, user- and environment- friend Propulsion System | 10 | confirmed | Mr. Luciano Battocchio | Czech Republic | |
Optimized orbit transfer of a Gravidyne with low-thrust propulsion | 10 | confirmed | Mr. David Gil | United Arab Emirates University (UAEU) | United Arab Emirates |
10 | confirmed | Mr. Vincent Ugolini | Korea Advanced Institute of Science and Technology (KAIST) | Korea, Republic of | |
The Turborocket Engine: An Integrated Pump-Fed Rocket Engine for Propulsion Applications | 10 | withdrawn | Dr. John Bossard | United States | |
Physical properties and ignition characteristics of hypergolic propellant with oxidizing additives | 10 | confirmed | Mr. Kyounghwan Lee | Hanbat National University | Korea, Republic of |
ignition delay and thermoacoustic coupling in hybrid rocket combustion | 10 | confirmed | Prof. Changjin Lee | Konkuk University | Korea, Republic of |
two-phase, multicomponent hydrogen peroxide blowdown injector modelling and tests comparisons | 10 | confirmed | Mr. Arthur Bahdur | Alcântara Launch Center | Brazil |
Wave Steepening Instability Caused by Hypergolic Detonation of High Test Peroxide-based Hypergol | 10 | withdrawn | Mr.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 |
10 | confirmed | Mr. B Deependran | Indian Space Research Organization (ISRO) | India | |
Designing a nuclear electric propulsion system for future Pluto missions | 10 | confirmed | Mr. Maanyash Jain | India | |
10 | Prof. Olexandr Petrenko | Flight Control LLC | Ukraine | ||
10 | confirmed | Mr. Jonathan Johnson | The University of Alabama | United States | |
10 | confirmed | Mr. Riccardo Gelain | Université Libre de Bruxelles | Belgium | |
10 | confirmed | Mr. Nicolás de Jong | LEEM-UPM | Spain | |
10 | confirmed | Ms. Aarya Kulkarni | International Space University (ISU) | India | |
10 | confirmed | Mr. Mahir Rawal | India | ||
The Relativistic Mass Ratio in Ultrarelativistic Photon Rockets | 10 | Prof. Espen Haug | Norwegian University of Science and Technology | Norway | |
Simulation analysis of multimode propulsion systems for satellites | 10 | withdrawn | Ms. Sagarika Rao Valluri | RNSIT Bangalore | India |
10 | confirmed | Dr. Jayakumar Venkatesan | Valles Marineris International Private Limited | India | |
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 |
Aerodynamic analysis on JAXA’s experimental vehicle for hypersonic flight | 10 | Dr. Susumu Hasegawa | Japan Aerospace Exploration Agency (JAXA) | Japan | |
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 |
Three-Dimensional MHD Analysis of Magnetic Plasma Drag with Coils Placed on Three Axes | 10 | confirmed | Dr. Shoko Arita | Shizuoka University | Japan |
10 | confirmed | Dr. Egor Loktionov | Bauman Moscow State Technical University | Russian Federation | |
A Novel Design Usage of Thermoelectric Materials in Aerospike Engines | 10 | confirmed | Mr. Gautam Arora | University of Petroleum and Energy Studies | India |
10 | confirmed | Mr. Priyank Dubey | Indian Institute of Technology | India | |
The nano-probe by the photon transportation in the Deep Space | 10 | confirmed | Mr. Jamel Metmati | THALES Services | France |
9tonf staged combustion cycle liquid rocket engine startup analysis | 10 | confirmed | Mrs. BOYEON KHIM | Korea, Republic of | |
10 | confirmed | Mr. Vignesh G | ISRO Propulsion Complex, Mahendragiri, India | India | |
10 | confirmed | Mr. Danylo Shcherbak | Flight Control LLC | Ukraine | |
10 | confirmed | Mr. ILYES GHEDJATTI | Beijing University of Aeronautics and Astronautics (BUAA) | China | |
cold-gas experiments on advanced nozzles in subsonic counter-flows | 10 | withdrawn | Mr. Giuseppe Scarlatella | Technische Universität Dresden (DTU) | Germany |
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 |
The effect of aerodynamic heating to cryogenic propellant discharge | 10 | confirmed | Dr. Seungwhan Baek | Korea Aerospace Research Institute (KARI) | Korea, Republic of |
10 | confirmed | Mr. Rawoof Shaik | University of Pisa | Italy | |
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 |
Rapid Design of a Small Scale KeroLOx Flight Vehicle Propulsion System | 10 | confirmed | Mr. Nathan Hirsch | Viterbi School of Engineering, USC | United States |
FEASIBILITY ANALYSIS FOR ELECTRIC PROPULSION SYSTEMS FOR SHORT TERM INTERPLANETARY MISSIONS | 10 | confirmed | Ms. Pritha Pal | University of Michigan | United States |
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 |
Computational model for performance prediction of a nitrous oxide / eicosane hybrid rocket engine | 10 | confirmed | Mr. Joel Jean-Philyppe | McGill University | Canada |
Common pitfalls of testing hybrid rocket engines at student led facilities | 10 | confirmed | Mr. Cyril Mani | McGill University | Canada |
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 |
Experimental & Numerical Investigation of GOx/GCH4 Combustion in a 7-Element Rocket Combustor | 10 | Mr. Abhishek Sharma | Indian Space Research Organization (ISRO) | India | |
10 | confirmed | Mr. Yuhang Li | Xi'an Aerospace Propulsion Institute | China | |
Integrated internal and external ballistics for sounding rocket design | 10 | confirmed | Dr. Jeongmoo Huh | United Arab Emirates University (UAEU) | United Arab Emirates |
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 |
10 | confirmed | Mr. Dhiyaneshwar L V | SASTRA University | India | |
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 |
Modeling of wall-bounded high pressure flows in Liquid Rocket Engines | 10 | Mr. Giuseppe Indelicato | Sapienza University of Rome | Italy | |
High Flux Hybrid Motor Development with Distributed Tube Injector | 10 | confirmed | Mr. Mehmet Kahraman | Deltav Space Technologies,Inc. | Türkiye |
Research on Acoustic Closed-End Device for Hydraulic Excitation Test of LRE | 10 | confirmed | Dr. meng dong | Xi'an Aerospace Propulsion Institute | China |
10 | confirmed | Dr. Marco Invigorito | CIRA Italian Aerospace Research Centre | Italy | |
10 | confirmed | Mr. Shutao Han | Beihang University (BUAA) | China | |
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 |
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 |
10 | confirmed | Mr. Norbert Szulc | Gdansk University of Technology | Poland | |
Using differential pressure sensor to measure nitrous oxide level in a tank | 10 | confirmed | Mr. Mateusz Czapski | Gdansk University of Technology | Poland |