session IP
- Title
Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM
- type
interactive
- Description
This session offers a unique opportunity to deliver your key messages in an interactive presentation on any of the subjects of Space Propulsion addressed in the classic Sessions. The presentation will be displayed on a digital screen in a dedicated location and available for view by all Congress attendees for the entire Congress week. In addition, one afternoon is dedicated exclusively for the attendees to view the Interactive Presentations, and the author will be assigned a specific ten minute slot to personally present the topic and interact with the attendees present. The Interactive Presentation may take advantage of all electronic display capabilities, such as: PowerPoint charts, embedded hot links, pictures, audio and video clips etc. An award will also be presented to the author of the best Interactive Presentation in the C Category at a special ceremony. An Abstract that follows the standard format must be submitted by the deadline for standard IAC abstracts.
- Room
- IPC members
Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;
Co-Chair: Mr. Andrei Shumeiko, Bauman Moscow State Technical University, Russian Federation;
Co-Chair: Prof. Riheng Zheng, Beihang University, China;
Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|
10 | confirmed | Mr. Jung-Won Kuk | Soletop CO., Ltd | Korea, Republic of | |
10 | withdrawn | Mr. Yiğit Kılıçaslan | Samsun University | Türkiye | |
10 | confirmed | Mr. Denis Egoshin | Bauman Moscow State Technical University | Russian Federation | |
10 | Mr. gildo di domenico | Research Consortium Hypatia | Italy | ||
Advancements in Hall Effect Thruster Design for Optimizing Performance in Space Missions: A Review | 10 | withdrawn | Ms. Yashika Paharia | University of Petroleum and Energy Studies | India |
Computational Simulation of Neutral Gas Dynamics in the CubeSat Ambipolar Thruster | 10 | confirmed | Ms. Thamiris Thomazini Libard | University of Brasilia | Brazil |
10 | confirmed | Ms. Blanca Pavón-Castillo | Xiroi Aerospace | Spain | |
10 | confirmed | Mr. Max Amer | Universitat Politecnica de Catalunya (UPC BarcelonaTech) | Spain | |
Fabrication and Testing of Applied Field Magneto Plasma Dynamic Thruster with Argon as Propellant | 10 | confirmed | Mr. Akash C | Hindustan Univerisity | India |
10 | Mr. Chenxi Xia | Beihang University (BUAA) | China | ||
10 | confirmed | Mr. Adrià Barceló | Universitat Politecnica de Catalunya (UPC BarcelonaTech) | Spain | |
stargate: an undergraduate experimental electric propulsion student research project | 10 | confirmed | Ms. Claude Blue | University of Alabama in Huntsville | United States |
Designing a nuclear electric propulsion system for future Pluto missions | 10 | confirmed | Mr. Gourav Mohanan | Dayananda Sagar University | India |
Design and structural analysis of low-cost modular rocket engine test stand. | 10 | confirmed | Mr. Michał Kret | Warsaw University of Technology (WUT) | Poland |
10 | confirmed | Mr. Claudio Antonio Morales Benítez | High Technology Unit (UAT) Faculty of Engineering - UNAM | Mexico | |
10 | confirmed | Mr. Alan Adan Velazquez Samaniego | Instituto Tecnológico de Durango (ITD) | Mexico | |
A Study on the Optimum Design of Solid Propellant Grain Using Machine Learning. | 10 | withdrawn | Mr. JINSEOK YOO | Inha Univ. | Korea, Republic of |
10 | confirmed | Mr. Giorgio Appignanesi | ISAE - Institut Supérieur de l'Aéronautique et de l'Espace | France | |
Innovative Methodology for Evaluating Combustion Efficiency in Swirled Rocket Engines | 10 | confirmed | Mr. Valerio Santolini | Politecnico di Milano | Italy |
10 | confirmed | Mr. XIAOTING NIU | Beihang University (BUAA) | China | |
10 | confirmed | Mr. Gustavo Callai | University of Brasilia | Brazil | |
10 | confirmed | Mr. Michał Kret | Warsaw University of Technology (WUT) | Poland | |
Analysis of the nozzle impact on the characteristics of the pulse detonation engine | 10 | confirmed | Mr. Oleksandr Aksonov | Yuzhnoye State Design Office | Ukraine |
10 | confirmed | Prof. Rachid Amrousse | Chouaib Doukkali University | Morocco | |
10 | confirmed | Mr. Elia Puccinelli | University of Pisa | Italy | |
10 | confirmed | Mr. Zelalem Bogale | Ethiopian Space Science and Technology Institute (ESSTI) | Ethiopia | |
Development and validation of rocket motor simulation software | 10 | confirmed | Mr. Michał Tomporowski | Warsaw University of Technology (WUT) | Poland |
10 | Mr. Ishaan Dutta | R V College of Engineering, Bengaluru | India | ||
10 | Mr. Om Kiritbhai Daxini | R V College of Engineering, Bengaluru | India | ||
Developments in additive manufacturing for \\ solid and hybrid rocket propulsion charges | 10 | withdrawn | Prof. Filippo Maggi | Politecnico di Milano | Italy |
10 | confirmed | Mr. Xiaoming Gu | Beihang University (BUAA) | China | |
Effect of manufacturing parameters on tungsten microstructures as an emitter for FEEP thrusters | 10 | confirmed | Mr. Jung Won Kuk | Soletop CO., Ltd | Korea, Republic of |
10 | confirmed | Mrs. Aneta Krawiec | Wroclaw University of Science and Technology | Poland | |
Fluidic throat technology for hybrid rocket motor based on liquid oxidizer cooling | 10 | confirmed | Dr. Haizhou Guo | Beihang University (BUAA) | China |
Hydro-thermal Analysis of Fuel Element of a Nuclear Thermal Engine | 10 | withdrawn | Ms. Nandini Sachdev | University of Petroleum and Energy Studies | India |
Introduction of Field Emission Electric Propulsion Research in Republic of Korea | 10 | confirmed | Prof. Kyun Ho Lee | Sejong University | Korea, Republic of |
INVESTIGATION INTO THE SUITABLE INJECTOR TYPES FOR SMALL-SCALE GASEOUS THRUST CHAMBERS | 10 | confirmed | Mr. Mousa Aqailan | United Arab Emirates University (UAEU) | United Arab Emirates |
10 | confirmed | Mr. Yudong Lu | Beihang University | China | |
10 | confirmed | Mr. Basel Altawil | Khalifa University of Science and Technology (KUST) | United Arab Emirates | |
10 | confirmed | Dr. abderrahim Nabi | Khalifa University of Science and Technology (KUST) | United Arab Emirates | |
Numerical Computations of Nozzle Performance Losses in Solid Rocket Motors | 10 | confirmed | Mr. Gianluca Cocirla | Sapienza University of Rome | Italy |
10 | confirmed | Mr. Ruikai Chen | Beihang University (BUAA) | China | |
10 | confirmed | Dr. Xintong Li | Beihang University (BUAA) | China | |
10 | confirmed | Mr. Mohd.Amaan Mukadam | SRM Institute of Science and Technology | India | |
10 | confirmed | Mr. Osmar Naim Corona Zamudio | High Technology Unit (UAT) Faculty of Engineering - UNAM | Mexico | |
Performance testing of small scale resistojet thruster with 3D printed heat exchanger | 10 | confirmed | Mr. Abdallah Alazeezi | United Arab Emirates University (UAEU) | United Arab Emirates |
10 | Mr. WENBO DONG | Shanghai Academy of Spaceflight Technology (SAST), China Aerospace and Technology Corporation (CASC) | China | ||
Research on cryogenic line chill-down process of industrial Teflon coated piping | 10 | confirmed | Mr. Hyunjun Kim | Korea Aerospace Research Institute (KARI) | Korea, Republic of |
10 | confirmed | Ms. Małgorzata Majda | Gdansk University of Technology | Poland | |
10 | confirmed | Mr. Camilo Sierra | Universidad de Antioquia | Colombia | |
10 | confirmed | Prof.Dr. José Rocco | ITA-DCTA | Brazil | |
10 | confirmed | Mr. Won Gyo Seo | Soletop CO., Ltd | Korea, Republic of | |
development of subcooled liquid oxygen system for liquid rocket engine | 10 | confirmed | Mr. JANGHWAN LEE | Korea Aerospace Research Institute (KARI) | Korea, Republic of |
Fatigue Failure Mechanism of Metal Bellows Caused by Flow-Induced Vibrations | 10 | withdrawn | Mr. Zitao WANG | Beijing Institute of Astronautical Systems Enginnering | China |
Thermal Decomposition of Hydrogen Peroxide (H2O2) in the Lab-scale for Space Applications | 10 | confirmed | Prof. Rachid Amrousse | Chouaib Doukkali University | Morocco |
10 | confirmed | Mr. Marco Cárdenas Aldaco | Administración de Sistemas Aeroespaciales Mexicanos - ASAEM | Mexico | |
thermal responsive propellant formulations for variable thrust control for winged space rocket | 10 | confirmed | Ms. Diana ALjbour | Space Generation Advisory Council (SGAC) | Jordan |
Numerical Design Optimization of a Blow-Down Supersonic Wind Tunnel | 10 | confirmed | Dr. Riccardo Nicoletti | Scuola di Ingegneria Aerospaziale "La Sapienza" | Italy |
10 | withdrawn | Mr. Vincenzo Castrignano | Università degli Studi di Napoli “Federico II” | Italy | |
hybrid propulsion system for spaceplanes: optimizing efficiency and performance | 10 | confirmed | Ms. Diana ALjbour | Space Generation Advisory Council (SGAC) | Jordan |
10 | Ms. Laurine Hillion | Hybrid Propulsion for Space (HyPr Space) | France | ||
10 | confirmed | Mr. Omar ElSherbiny | Technical University of Munich | Germany | |
10 | confirmed | Mr. Colum Walter | Universität der Bundeswehr München | Germany | |
10 | confirmed | Mr. Marek Dzik | Warsaw University of Technology (WUT) | Poland | |
Conceptual development of modular ion thrusters for its use on nuclear electric propulsion systems. | 10 | confirmed | Mr. Oscar Mejia | Instituto Politécnico Nacional | Mexico |
10 | confirmed | Mr. Alessandro Battegazzore | Delft University of Technology (TU Delft) | The Netherlands | |
SRAD Capacitive Level Sensor for Propellant Measurement of a Liquid Rocket | 10 | confirmed | Ms. Sheikha Al-Nasser | Propulse NTNU | Norway |
Propulsion systems for Mars mission: alternatives and opportunities | 10 | confirmed | Ms. Sai Susmitha Guddanti | Department of Space Studies, University of North Dakota | United States |
10 | confirmed | Mr. matteo crachi | Politecnico di Torino | Italy | |
Investigation of Hypergolic Ignition of Green Kerosene-based Fuels with HTP | 10 | confirmed | Mr. Luca Caffiero | Politecnico di Milano | Italy |
10 | confirmed | Mr. Shayman-Reza Labadlia | Concordia University | Canada | |
10 | withdrawn | Mr. Alberto Sarritzu | University of Pisa | Italy | |
10 | confirmed | Mr. Alejandro Guerra Mentruit | GTD | Spain | |
Durable oxide catalysts free of noble metals for Hydrogen peroxide thrusters | 10 | confirmed | Dr. Stefano Mungiguerra | Università degli Studi di Napoli “Federico II” | Italy |
Design of a Propellant Liquefaction and Storage System for Cryogenic Rocket Engine Propellants | 10 | confirmed | Dr. Alejandro Hernandez Gonzalez | Technische Universität München | Mexico |
10 | withdrawn | Mr. Shreyansh Dubey | University of Petroleum and Energy Studies | India | |
A novel technique for salvaging a double walled thrust chamber nozzle | 10 | confirmed | Mr. Vivek S | Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC) | India |
10 | confirmed | Mr. Haoran Shi | School of Astronautics, Beihang University | China | |
10 | confirmed | Mr. Chenxi Xia | Beihang University (BUAA) | China | |
10 | confirmed | Mr. Vishal Singh | Bellatrix Aerospace Private Limited | India | |
10 | confirmed | Mr. Vincent Ugolini | Korea Advanced Institute of Science and Technology (KAIST) | Korea, Republic of | |
Closed-Loop Thrust Throttling Capabilities on Kero-Lox Liquid Rocket Engine | 10 | confirmed | Mr. Connor Zook | University of Southern California | United States |
combustion characteristics of hydroxylammonium nitrate-based electrically controlled gel propellant | 10 | confirmed | Ms. CHANSONG KIM | Chosun University | Korea, Republic of |
10 | confirmed | Mr. Federico Giambelli | Politecnico di Milano | Italy | |
10 | confirmed | Mr. Antonio Lioi | Sidereus Space Dynamics | Italy | |
10 | confirmed | Mr. Dae Hwan Kim | Seoul National University | Korea, Republic of | |
10 | withdrawn | Mr. Timothy Velthuysen | University of KwaZulu-Natal (UKZN) | South Africa | |
Conceptual Design and Fabrication of 400 N-class Multi-hole Pintle GCH4/LOx Injector | 10 | confirmed | Mr. YOONHO SONG | Korea Aerospace Research Institute (KARI) | Korea, Republic of |
10 | confirmed | Dr. Djamal DARFILAL | Khalifa University of Science and Technology (KUST) | United Arab Emirates | |
10 | confirmed | Dr. Djamal DARFILAL | Khalifa University of Science and Technology (KUST) | United Arab Emirates | |
10 | confirmed | Mr. Adil Mahroof | United Arab Emirates University (UAEU) | United Arab Emirates | |
Catalyst-Driven Green Propellant Development for Hypergolic Systems | 10 | confirmed | Prof. Rene Gonçalves | Aeronautic Institute of Technology (ITA) | Brazil |
Characterization of Engine Cooldown for a Centrifugal Nuclear Thermal Rocket | 10 | confirmed | Mr. Mitchell Schroll | Propulsion Research Center, University of Alabama in Huntsville | United States |
Thermal Considerations of Vaporization in Liquid Core Nuclear Thermal Rockets | 10 | withdrawn | Mr. Dakota Santana | University of Alabama in Huntsville | United States |
10 | confirmed | Dr. Lorenzo Niccolai | University of Pisa | Italy | |
10 | confirmed | Dr. Ryan Weed | United States | ||
innovations in nuclear and propellantless propulsion technologies | 10 | confirmed | Mr. Ali Jafarov | National Aviation Academy - Azerbaijan | Azerbaijan |
molten salt reactor concepts for advanced nuclear electric propulsion (NEP) systems | 10 | confirmed | Prof. Pablo Rubiolo | CNRS-INPG-UJF | France |
Review of Nuclear Electric Propulsion for Interplanetary Missions | 10 | confirmed | Mrs. Monica Salunkhe | University of Alabama in Huntsville | United States |
10 | withdrawn | Mrs. Monica Salunkhe | University of Alabama in Huntsville | United States | |
Hydrolytic space propulsion: \\ a new opportunity for cubesat missions | 10 | confirmed | Prof. Filippo Maggi | Politecnico di Milano | Italy |
Optimising Solar Sail Design for Interplanetary Missions: Balancing Mass, Area, and Trajectory | 10 | confirmed | Ms. SUHANA ARSH | R V College of Engineering, Bengaluru | India |
THE GREEN FUTURE OF PROPULSION FOR SATELLITES & SPACE VEHICLES | 10 | Mr. Sergii Kamenskyi | Spain | ||
10 | confirmed | Mr. Vadym Khomiak | Yuzhnoye State Design Office | Ukraine | |
Preliminary Test of Kerosene Nitrous Oxide Catalytic Decomposition Bipropellant Thruster | 10 | withdrawn | Dr. Seungho Lee | Korea Aerospace Research Institute (KARI) | Korea, Republic of |
Preliminary study on an electrolysis-based satellite micropropulsor for a 12U cubesat | 10 | confirmed | Mr. Nicolás de Jong | Spain | |
Perspectives on Colloidal Polymeric Nitrogen Monopropellant Engines | 10 | confirmed | Mr. Davide Negretti | Italy | |
Optimization study of an upper stage based on an e-pump-fed engine | 10 | confirmed | Mr. Andrea Montaini | Politecnico di Milano | Italy |
Optimization of thrust control strategy for electric pump-fed rocket engines | 10 | confirmed | Mr. Tianwen Li | School of Astronautics, Beihang University | China |
10 | confirmed | Mr. Francesco Marino | Capsule Corporation | Italy | |
10 | confirmed | Dr. Wenbing Jiang | Aerospace System Engineering Shanghai, China | China | |
Integrated propulsion control technology for Future Space Transportation Systems | 10 | Mr. Wang Tempo | China Aerospace Science and Technology Corporation (CASC) | China | |
In house development of novel, thermally stable ceramic composite catalyst for HAN Decomposition | 10 | Dr. Rekha M | Bellatrix Aerospace Private Limited. | India | |
fault simulation study of full-flow staged combustion cycle engine start-up process | 10 | confirmed | Mr. Lihao Zheng | School of Astronautics, Beihang University | China |
10 | confirmed | Mr. liu yuwei | National University of Defense Technology | China | |
Digital Twin Performance Analysis of a 500 pound-thrust, Throttling, Hypergolic Rocket Engine | 10 | confirmed | Mr. Clayton Birchenough | United States | |
Development of Atlas: A Liquid Rocket Engine Cryogenic Feed System | 10 | confirmed | Mr. Sebastian Bouckenooghe | University of Southern California | United States |
10 | confirmed | Mr. Tommaso Zagatti | Telematic Solutions Srl | Italy | |
Design and evaluation of a small scale liquid rocket engine using pineapple’s waste | 10 | confirmed | Mr. Alvaro Bermudez | University of Costa Rica | Costa Rica |
Design and Analysis of a LH2-LOX Rotating Detonation Propulsion System | 10 | confirmed | Mr. Sihan Di | School of Astronautics, Beihang University | China |
BREAKING BARRIERS WITH BIOFUELS: THE FUTURE OF ROCKET PROPULSION | 10 | confirmed | Ms. Vanmitha Athimoolam | Malaysia | |
Establishing a Foundation for Rocketry Advancement in Mexico: Development of a Hybrid Rocket Engine. | 10 | confirmed | Mr. Luis Fernando Gomez Monroy | Mexico | |
Hybrid Rocket Simulation Using CEQUEL for Thermochemistry Calculations | 10 | confirmed | Ms. Paige Berg | University of Alabama in Huntsville | United States |
Fundamental Investigation of Micro-Explosive in Aluminum-Lithium Alloy Particle at the Atomic Scale | 10 | confirmed | Mr. Yintao Zhou | Beijing Institute of Technology (BIT) | China |
Performance analysis of Paraffin, Beeswax and Magnesium as a fuel for Hybrid Propulsion | 10 | confirmed | Mr. Harish Vernekar | University of Arizona | United States |
10 | confirmed | Dr. ANWER HASHISH | Military Technical College | Egypt | |
Conceptual design of a 1 kN hybrid rocket engine manufactured with additive technology | 10 | confirmed | Dr. Olexiy Shynkarenko | University of Brasilia | Brazil |
Numerical modelling approach for the development of an orbital-scale hybrid propulsion engine | 10 | confirmed | Mr. Vishesh Garg | Hybrid Propulsion for Space (HyPr Space) | France |
advancing thermal management: heat flow analysis and hotspot identification in solid rocket motors | 10 | Mr. Kushal Chatterjee | R V College of Engineering, Bengaluru | India | |
Thrust Prediction of Hybrid Rocket Motor Based on Physical Feature Embedding and Residual Learning | 10 | confirmed | Dr. Weile Xu | Beihang University (BUAA) | China |
Statistical Thermodynamics Approaches for Advancing Chemical Propulsion Systems | 10 | Mr. Ishaan Dutta | R V College of Engineering, Bengaluru | India | |
Research on charge integrity simulation of brush charge asymmetric ignition of small solid thruster | 10 | confirmed | Mr. Yuqing Tang | Nanjing University of Science and Technology | China |
10 | confirmed | Mr. Abishek Shrestha | Space Generation Advisory Council (SGAC) | Australia | |
NUMERICAL AND EXPERIMENTAL ANALYSIS OF NEW PROPELLANT FORMULATIONS FOR HYBRID ROCKETS | 10 | confirmed | Mr. Abdul Rahman | Scuola di Ingegneria Aerospaziale "La Sapienza" | Italy |
10 | withdrawn | Mrs. Keren Lin | Beihang University (BUAA) | China | |
H2O2/HDPE Hybrid Rocket: Experimental and Theoretical Investigation | 10 | confirmed | Mr. Abdul Rahman | Scuola di Ingegneria Aerospaziale "La Sapienza" | Italy |
Development of Carbon Fiber Rocket Motors with Insulative Laminate Structure | 10 | Mr. Ishaan Dutta | R V College of Engineering, Bengaluru | India | |
AI and Classical Approaches to Estimating Solid Fuel Regression Rate in Hybrid Rocket Engines | 10 | confirmed | Mr. Gabriel Metre Resende | University of Brasilia | Brazil |