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  • session IP

    Title

    Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

    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

    IP Area (Hall B)

    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;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    A Study of Prediction and Validation of FEEP Crown needle Internal Porosity for small satellites using CNN(Convolutional Neural Network) and random functions

    10

    confirmed

    Mr. Jung-Won Kuk

    Soletop CO., Ltd

    Korea, Republic of

    2

    EFFECT OF EXPANDED COOLING CHANNELS ON THE THERMAL AND STRUCTURAL STRENGTH OF THE MATERIALS USED IN HYBRID ROCKET ENGINES

    10

    confirmed

    Mr. Yiğit Kılıçaslan

    Samsun University

    Türkiye

    3

    INFLUENCE OF SURFACE AREA AND PROPELLANT MATERIAL ON THE IMPULSE BIT IN ABLATIVE PULSE PLASMA ACELERATOR

    10

    confirmed

    Mr. Denis Egoshin

    Bauman Moscow State Technical University

    Russian Federation

    4

    Sprite-Class Satellites Propulsion to Extended Lifespan

    10

    Mr. gildo di domenico

    Research Consortium Hypatia

    Italy

    5

    Advancements in Hall Effect Thruster Design for Optimizing Performance in Space Missions: A Review

    10

    Ms. Yashika Paharia

    University of Petroleum and Energy Studies

    India

    6

    Computational Simulation of Neutral Gas Dynamics in the CubeSat Ambipolar Thruster

    10

    Ms. Thamiris Thomazini Libard

    University of Brasilia

    Brazil

    8

    Development and Preliminary Evaluation of Plugim Electrospray Thruster: Focus on the Fuel Management System and Power Processing Unit

    10

    confirmed

    Ms. Blanca Pavón-Castillo

    Xiroi Aerospace

    Spain

    9

    Experimental Testing and Numerical Simulation Validation of an Air Intake for Air-Breathing Electric Propulsion (ABEP) Systems

    10

    confirmed

    Mr. Max Amer

    Universitat Politecnica de Catalunya (UPC BarcelonaTech)

    Spain

    10

    Fabrication and Testing of Applied Field Magneto Plasma Dynamic Thruster with Argon as Propellant

    10

    confirmed

    Mr. Akash C

    Hindustan Univerisity

    India

    11

    Geometric characteristics optimization and integrated design analysis of Air-Breathing Electric Propulsion inlet

    10

    Mr. Chenxi Xia

    Beihang University (BUAA)

    China

    13

    optimisation and durability assessment of rf helicon-based plasma thruster (k-2) for very low earth orbit air-breathing electric propulsion

    10

    confirmed

    Mr. Adrià Barceló

    Universitat Politecnica de Catalunya (UPC BarcelonaTech)

    Spain

    14

    stargate: an undergraduate experimental electric propulsion student research project

    10

    confirmed

    Mr. Claude Blue

    University of Alabama in Huntsville

    United States

    15

    Designing a nuclear electric propulsion system for future Pluto missions

    10

    confirmed

    Mr. Sukhjit Singh

    Space Generation Advisory Council (SGAC)

    India

    16

    Design and structural analysis of low-cost modular rocket engine test stand.

    10

    confirmed

    Mr. Korneliusz Szalkowski

    Warsaw University of Technology (WUT)

    Poland

    16

    Improving rocket nozzle efficiency with rough surfaces

    10

    Mr. Claudio Antonio Morales Benítez

    High Technology Unit (UAT) Faculty of Engineering - UNAM

    Mexico

    17

    Power Sustainment in Long-Duration Space Missions through the Utilization of Nitinol Material Implemented in the Design of Solar Sails, Programmed with PID Control.

    10

    confirmed

    Mr. Alan Adan Velazquez Samaniego

    Instituto Tecnológico de Durango (ITD)

    Mexico

    18

    A Study on the Optimum Design of Solid Propellant Grain Using Machine Learning.

    10

    confirmed

    Mr. JINSEOK YOO

    Inha Univ.

    Korea, Republic of

    19

    Advancements in the development of the subsystems for a student-developed H2O2/ABS hybrid propellant rocket engine

    10

    Ms. Raquel Arrontes Quiroga

    ISAE - Institut Supérieur de l'Aéronautique et de l'Espace

    France

    20

    Alternative thrust-based algorithm for performance analysis of swirled hybrid rocket engines

    10

    confirmed

    Mr. Valerio Santolini

    Politecnico di Milano

    Italy

    21

    An Improved Al Particle Combustion Model for Simulating the Aluminized Hybrid Rocket Motor Combustion

    10

    confirmed

    Mr. XIAOTING NIU

    Beihang University (BUAA)

    China

    22

    Characterization of Paraffin-LDPE Blended Fuels

    10

    confirmed

    Mr. Rafael Coelho

    University of Brasilia

    Brazil

    23

    design of dual-bell nozzle specified for the second stage engine of students' designed sounding rocket

    10

    confirmed

    Mr. Michał Kret

    Warsaw University of Technology (WUT)

    Poland

    24

    Analysis of the nozzle impact on the characteristics of the pulse detonation engine

    10

    confirmed

    Mr. Oleksandr Aksonov

    Yuzhnoye State Design Office

    Ukraine

    25

    Decomposition mechanism of ammonium dinitramide: a sustainable energetic molecule for green propellant technologies

    10

    confirmed

    Mr. Zakaria Harimech

    Chouaib Doukkali University

    Morocco

    26

    Development and Integration of the Engineering Model for a Modular HTP-based CubeSat Propulsion System for future In-Orbit Validation on the UniPi EXCITE CubeSat Platform

    10

    confirmed

    Mr. Matteo Serchi Masini

    University of Pisa

    Italy

    27

    Development and Testing of an Electrically-Driven Centrifugal Pressurization System for Hybrid Rockets in Rocket Propulsion

    10

    confirmed

    Mr. Zelalem Bogale

    Ethiopian Space Science and Technology Institute (ESSTI)

    Ethiopia

    28

    Development and validation of rocket motor simulation software

    10

    confirmed

    Mr. Michał Tomporowski

    Warsaw University of Technology (WUT)

    Poland

    29

    Development of Environmentally Friendly Solid Propellants Using Fused Deposition Modeling Additive Manufacturing

    10

    Mr. Ishaan Dutta

    R V College of Engineering, Bengaluru

    India

    30

    Development of High-Performance Solid Rocket Propellants Using AP-HTPB Composite Matrix AND Different Plasticizers

    10

    Mr. Om Kiritbhai Daxini

    R V College of Engineering, Bengaluru

    India

    31

    Developments in additive manufacturing for \\ solid and hybrid rocket propulsion charges

    10

    withdrawn

    Prof. Filippo Maggi

    Politecnico di Milano

    Italy

    32

    Dynamic characteristics of hydrogen peroxide electric pump during pulse ignition process of hybrid rocket engine

    10

    confirmed

    Mr. Xiaoming Gu

    Beihang University (BUAA)

    China

    33

    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

    34

    Energetic co-crystals containing ammonium nitrate obtained by solvent method as an alternative to solid rocket fuels based on perchlorates

    10

    confirmed

    Mrs. Aneta Krawiec

    Wroclaw University of Science and Technology

    Poland

    35

    Fluidic throat technology for hybrid rocket motor based on liquid oxidizer cooling

    10

    confirmed

    Dr. Haizhou Guo

    Beihang University (BUAA)

    China

    36

    Hydro-thermal Analysis of Fuel Element of a Nuclear Thermal Engine

    10

    confirmed

    Ms. Nandini Sachdev

    University of Petroleum and Energy Studies

    India

    37

    Introduction of Field Emission Electric Propulsion Research in Republic of Korea

    10

    confirmed

    Prof. Kyun Ho Lee

    Sejong University

    Korea, Republic of

    38

    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

    39

    Investigation of Solid Fuel Pyrolysis Characteristics in Hybrid Rocket Engines Utilizing HTPB with Aluminum Additive

    10

    Mr. Yudong Lu

    Beihang University

    China

    40

    Low-cost Innovative Experimental Setup for Assessing Laser-Driven Propulsion in Near-Ultimate Vacuum Conditions

    10

    confirmed

    Mr. Basel Altawil

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    41

    Maximizing Reusability in Propulsion System Testing: A modular Data Acquisition System Using National Instruments PXI hardware and LabVIEW

    10

    confirmed

    Dr. abderrahim Nabi

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    42

    Numerical Computations of Nozzle Performance Losses in Solid Rocket Motors

    10

    confirmed

    Dr. Marco Grossi

    Sapienza University of Rome

    Italy

    43

    Numerical Simulation and Experimental Study of the Throat Parallel Segment Length of Variable Area Cavitating Venturi

    10

    confirmed

    Mr. Ruikai Chen

    Beihang University (BUAA)

    China

    44

    Optimization of pump-valve combined regulation strategy for electric pump-fed system in a hybrid rocket motor

    10

    confirmed

    Dr. Xintong Li

    Beihang University (BUAA)

    China

    45

    Optimizing Launch Systems: Propulsion and Structural Innovations for Enhanced Efficiency in Advanced Vehicles

    10

    confirmed

    Mr. Mohd.Amaan Mukadam

    SRM Institute of Science and Technology

    India

    46

    pace hybrid propulsion: a combination of electric and thermonuclear propulsion to optimize satellites

    10

    confirmed

    Mr. Osmar Naim Corona Zamudio

    High Technology Unit (UAT) Faculty of Engineering - UNAM

    Mexico

    47

    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

    49

    research on mechanism for high nozzle closure opening pressure of solid rocket motor in stage separation

    10

    Mr. WENBO DONG

    Shanghai Academy of Spaceflight Technology (SAST), China Aerospace and Technology Corporation (CASC)

    China

    50

    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

    51

    Research on the performance of the modified paraffin-wax-based fuel grains in the use of Student Researched and Developed (SRAD) hybrid rocket motor

    10

    confirmed

    Mr. Maciej Zawadzki

    Gdansk University of Technology

    Poland

    52

    research, analysis and experimental development of solid propellant type rnx for rocket engines in environments with humid mountain climate

    10

    confirmed

    Mr. Daniel Cardenas

    Universidad de Antioquia

    Colombia

    53

    RMD simulations applied to the study of energetic materials like HMX smokeless solid propellant: a case study of HMX molecular vacancies.

    10

    confirmed

    Prof.Dr. José Rocco

    ITA-DCTA

    Brazil

    54

    Systemisation and Performance Testing of Field Emission Electric Propulsion Thruster using Gallium as Propellant

    10

    confirmed

    Mr. Won Gyo Seo

    Soletop CO., Ltd

    Korea, Republic of

    55

    development of subcooled liquid oxygen system for liquid rocket engine

    10

    confirmed

    Mr. JANGHWAN LEE

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    56

    Fatigue Failure Mechanism of Metal Bellows Caused by Flow-Induced Vibrations

    10

    confirmed

    Mr. Zitao WANG

    Beijing Institute of Astronautical Systems Enginnering

    China

    57

    Thermal Decomposition of Hydrogen Peroxide (H2O2) in the Lab-scale for Space Applications

    10

    confirmed

    Ms. Hajar Jabri

    Chouaib Doukkali University

    Morocco

    58

    design and cfd analysis of a hypersonic inlet and hydrogen combustion for a scramjet engine at mach 7

    10

    confirmed

    Mr. Marco Cárdenas Aldaco

    Administración de Sistemas Aeroespaciales Mexicanos - ASAEM

    Mexico

    59

    thermal responsive propellant formulations for variable thrust control for winged space rocket

    10

    confirmed

    Ms. Diana ALjbour

    Space Generation Advisory Council (SGAC)

    Jordan

    60

    MULTIDISCIPLINARY DESIGN OPTIMIZATION OF A SUPERSONIC WIND TUNNEL

    10

    confirmed

    Dr. Antonella Ingenito

    Sapienza University of Rome

    Italy

    61

    Modelling of Hypersonic Pre-cooled Engine

    10

    confirmed

    Mr. Vincenzo Castrignano

    Università degli Studi di Napoli “Federico II”

    Italy

    62

    hybrid propulsion system for spaceplanes: optimizing efficiency and performance

    10

    confirmed

    Ms. Diana ALjbour

    Space Generation Advisory Council (SGAC)

    Jordan

    63

    Enhancing the Performance of Solid-Fuel Dual Scramjet through Innovative Design and Numerical Investigation

    10

    Ms. Laurine Hillion

    Hybrid Propulsion for Space (HyPr Space)

    France

    64

    Development of an Air-Breathing Electrostatic Thruster

    10

    confirmed

    Mr. Omar ElSherbiny

    Technical University of Munich

    Germany

    65

    Plume characterization of a magnetic nozzle thruster by two-dimensional laser-induced fluorescence measurements

    10

    confirmed

    Mr. Colum Walter

    Universität der Bundeswehr München

    Germany

    67

    Swirl injectors in hybrid rocket engine - design, parameters validation and applicability in a N2O/ABS hybrid rocket booster

    10

    confirmed

    Mr. Marek Dzik

    Warsaw University of Technology (WUT)

    Poland

    68

    Conceptual development of modular ion thrusters for its use on nuclear electric propulsion systems.

    10

    confirmed

    Mr. Oscar Mejia

    Instituto Politécnico Nacional

    Mexico

    69

    Rapid iterative design of a cost-effective e-pump for a liquid-fuelled reusable sounding rocket: a comprehensive approach to in-house design, manufacturing and testing.

    10

    confirmed

    Mr. Alessandro Battegazzore

    Delft Aerospace Rocket Engineering (DARE)

    The Netherlands

    70

    SRAD Capacitive Level Sensor for Propellant Measurement of a Liquid Rocket

    10

    confirmed

    Ms. Sheikha Al-Nasser

    Propulse NTNU

    Norway

    71

    Propulsion systems for Mars mission: alternatives and opportunities

    10

    confirmed

    Dr. Marcos Fernandez-Tous

    Department of Space Studies, University of North Dakota

    United States

    72

    Life evaluation of liquid rocket engine regenerative cooling system: a comparison of hardening models

    10

    confirmed

    Mr. matteo crachi

    Politecnico di Torino

    Italy

    73

    Investigation of Hypergolic Ignition of Green Kerosene-based Fuels with HTP

    10

    confirmed

    Mr. Luca Caffiero

    Politecnico di Milano

    Italy

    74

    Full rotordynamics analysis of a turbopump rotor system

    10

    confirmed

    Mr. Shayman-Reza Labadlia

    Concordia University

    Canada

    75

    Feasibility Study and Preliminary Design of an Innovative Green Propulsion concept based on Self-Pressurized Propellants

    10

    withdrawn

    Mr. Alberto Sarritzu

    University of Pisa

    Italy

    76

    Enhancing Reliability in European Rocket Engines: The GTD Approach to Engine Test Bench Control and Monitoring at DLR Lampoldshausen

    10

    confirmed

    Mr. Alejandro Guerra Mentruit

    GTD

    Spain

    77

    Durable oxide catalysts free of noble metals for Hydrogen peroxide thrusters

    10

    confirmed

    Dr. Frederic Monteverde

    CNR - ISSMC

    Italy

    78

    Design of a Propellant Liquefaction and Storage System for Cryogenic Rocket Engine Propellants

    10

    confirmed

    Dr. Alejandro Hernandez Gonzalez

    Technische Universität München

    Mexico

    79

    Cellulose-Based Gel Propellants for Advanced Space Applications: Synthesis, Characterization, and Performance Optimization

    10

    confirmed

    Mr. Shreyansh Dubey

    University of Petroleum and Energy Studies

    India

    80

    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

    81

    Experimental Investigation on Pressure and Flow Regulation of Variable Area Cavitation Venturi in Pump-feed System

    10

    confirmed

    Mr. Haoran Shi

    School of Astronautics, Beihang University

    China

    82

    Geometric characteristics optimization and integrated design analysis of Air-Breathing Electric Propulsion inlet

    10

    confirmed

    Mr. Chenxi Xia

    Beihang University (BUAA)

    China

    83

    Experimental study and modelling of rise time in HAN based monopropellant thruster and its effect on chamber pressure oscillations

    10

    confirmed

    Mr. Vishal Singh

    Bellatrix Aerospace Private Limited

    India

    84

    optical visualization of fuel injector with flat spray nozzle of throttling test during H2O2/kerosene bipropellant thruster.

    10

    confirmed

    Mr. Vincent Ugolini

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    85

    Closed-Loop Thrust Throttling Capabilities on Kero-Lox Liquid Rocket Engine

    10

    confirmed

    Mr. Connor Zook

    University of Southern California

    United States

    86

    combustion characteristics of hydroxylammonium nitrate-based electrically controlled gel propellant

    10

    confirmed

    Ms. CHANSONG KIM

    Chosun University

    Korea, Republic of

    87

    Regenerative and Liquid Film Cooling: Development of a Unified Thermal Control Strategy in Liquid Rocket Engines

    10

    confirmed

    Mr. Federico Giambelli

    Politecnico di Milano

    Italy

    88

    Potential of Radial Turbines in Liquid Rocket Engines: a comparative study with classical axial Turbines

    10

    confirmed

    Mr. Antonio Lioi

    Italy

    89

    Dynamic combustion characteristics of the GOX/GCH4 pintle model combustor with different sizes of the mantle recirculation zone

    10

    confirmed

    Mr. Dae Hwan Kim

    Seoul National University

    Korea, Republic of

    90

    Formulation, Rheology and Atomization of Gelled Hydroxylammonium Nitrate (HAN) “Green” Monopropellant Ternary Mixtures

    10

    confirmed

    Mr. Timothy Velthuysen

    University of KwaZulu-Natal (UKZN)

    South Africa

    91

    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

    92

    Characterization and Testing of a 1N Green Monopropellant Micro-Thruster Produced Using Additive Manufacturing Technique

    10

    Dr. Djamal DARFILAL

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    93

    Design, Development and Testing of a Five-Thruster Multidirectional Resistojet Propulsion System for cubsats applications

    10

    Dr. Djamal DARFILAL

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    94

    Decomposition characteristics of hydrogen peroxide by external heat source in small scale monopropellant thrusters

    10

    confirmed

    Mr. Adil Mahroof

    United Arab Emirates University (UAEU)

    United Arab Emirates

    95

    Catalyst-Driven Green Propellant Development for Hypergolic Systems

    10

    confirmed

    Prof. Rene Gonçalves

    Aeronautic Institute of Technology (ITA)

    Brazil

    96

    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

    97

    Thermal Considerations of Vaporization in Liquid Core Nuclear Thermal Rockets

    10

    Mr. Dakota Santana

    University of Alabama in Huntsville

    United States

    98

    Optimal trajectories for a spacecraft propelled by an E-sail with piecewise inertially-fixed attitude

    10

    confirmed

    Dr. Lorenzo Niccolai

    University of Pisa

    Italy

    99

    A Levitated Displacement Interferometer Thrust Stand for Characterization of Propellantless Propulsion Concepts

    10

    confirmed

    Dr. Ryan Weed

    United States

    100

    innovations in nuclear and propellantless propulsion technologies

    10

    confirmed

    Mr. Ali Jafarov

    National Aviation Academy - Azerbaijan

    Azerbaijan

    101

    molten salt reactor concepts for advanced nuclear electric propulsion (NEP) systems

    10

    confirmed

    Prof. Pablo Rubiolo

    CNRS

    France

    102

    Review of Nuclear Electric Propulsion for Interplanetary Missions

    10

    confirmed

    Mrs. Monica Salunkhe

    University of Alabama in Huntsville

    United States

    103

    Preliminary Low Thrust Direct Trajectory Design Using Nuclear Electric Propulsion System for Rendezvous Missions to Jupiter

    10

    confirmed

    Mrs. Monica Salunkhe

    University of Alabama in Huntsville

    United States

    104

    Hydrolytic space propulsion: \\ a new opportunity for cubesat missions

    10

    confirmed

    Prof. Filippo Maggi

    Politecnico di Milano

    Italy

    105

    Optimising Solar Sail Design for Interplanetary Missions: Balancing Mass, Area, and Trajectory

    10

    Ms. SUHANA ARSH

    R V College of Engineering, Bengaluru

    India

    106

    THE GREEN FUTURE OF PROPULSION FOR SATELLITES & SPACE VEHICLES

    10

    Mr. Sergii Kamenskyi

    Spain

    107

    The features of LVexisting pressurization systems of propellant tanks and prospects of their development

    10

    confirmed

    Mr. Vadym Khomiak

    Yuzhnoye State Design Office

    Ukraine

    108

    Preliminary Test of Kerosene Nitrous Oxide Catalytic Decomposition Bipropellant Thruster

    10

    withdrawn

    Mr. Seungho Lee

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    109

    Preliminary study on an electrolysis-based satellite micropropulsor for a 12U cubesat

    10

    confirmed

    Mr. Nicolás de Jong

    LEEM-UPM

    Spain

    110

    Perspectives on Colloidal Polymeric Nitrogen Monopropellant Engines

    10

    confirmed

    Mr. Davide Negretti

    Italy

    111

    Optimization study of an upper stage based on an e-pump-fed engine

    10

    confirmed

    Mr. Andrea Montaini

    Politecnico di Milano

    Italy

    112

    Optimization of thrust control strategy for electric pump-fed rocket engines

    10

    confirmed

    Mr. Tianwen Li

    School of Astronautics, Beihang University

    China

    113

    Modeling, Simulation and Testing of an Innovative Engineering Model Water-based Propulsion Unit for Cubesats

    10

    confirmed

    Mr. Francesco Marino

    Capsule Corporation

    Italy

    114

    Investigation on an efficient thermal pressurization method for propellant tanks of cryogenic upper stage

    10

    confirmed

    Dr. Wenbing Jiang

    Aerospace System Engineering Shanghai, China

    China

    115

    Integrated propulsion control technology for Future Space Transportation Systems

    10

    Mr. Wang Tempo

    China Aerospace Science and Technology Corporation (CASC)

    China

    116

    In house development of novel, thermally stable ceramic composite catalyst for HAN Decomposition

    10

    Dr. Rekha M

    Bellatrix Aerospace Private Limited.

    India

    117

    fault simulation study of full-flow staged combustion cycle engine start-up process

    10

    confirmed

    Mr. Lihao Zheng

    School of Astronautics, Beihang University

    China

    118

    Dynamics modeling and simulation analysis of reusable high-pressure supplementary combustion liquid oxygen kerosene variable thrust rocket engine: Part I - Single point operating condition analysis

    10

    confirmed

    Mr. liu yuwei

    National University of Defense Technology

    China

    119

    Digital Twin Performance Analysis of a 500 pound-thrust, Throttling, Hypergolic Rocket Engine

    10

    confirmed

    Mr. Clayton Birchenough

    United States

    120

    Development of Atlas: A Liquid Rocket Engine Cryogenic Feed System

    10

    confirmed

    Mr. Rohin Pathak

    University of Southern California

    United States

    121

    Design, Modeling and Simulations of a High Pressure Cryogenic System for a Space Propulsion Test Facility

    10

    confirmed

    Mr. Tommaso Zagatti

    Telematic Solutions Srl

    Italy

    122

    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

    123

    Design and Analysis of a LH2-LOX Rotating Detonation Propulsion System

    10

    confirmed

    Mr. Sihan Di

    School of Astronautics, Beihang University

    China

    124

    BREAKING BARRIERS WITH BIOFUELS: THE FUTURE OF ROCKET PROPULSION

    10

    confirmed

    Ms. Vanmitha Athimoolam

    Malaysia

    125

    Establishing a Foundation for Rocketry Advancement in Mexico: Development of a Hybrid Rocket Engine.

    10

    confirmed

    Mr. Luis Fernando Gomez Monroy

    Mexico

    126

    Hybrid Rocket Simulation Using CEQUEL for Thermochemistry Calculations

    10

    Ms. Paige Berg

    University of Alabama in Huntsville

    United States

    129

    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

    131

    Performance analysis of Paraffin, Beeswax and Magnesium as a fuel for Hybrid Propulsion

    10

    confirmed

    Mr. Harish Vernekar

    University of Arizona

    United States

    132

    Experimental investigation of combustion instability inside lab-scale hybrid rocket motor with swirl injector

    10

    confirmed

    Dr. ANWER HASHISH

    Military Technical College

    Egypt

    133

    Conceptual design of a 1 kN hybrid rocket engine manufactured with additive technology

    10

    confirmed

    Dr. Olexiy Shynkarenko

    University of Brasilia

    Brazil

    134

    Numerical modelling approach for the development of an orbital-scale hybrid propulsion engine

    10

    confirmed

    Mr. Raphaël Aubry

    Hybrid Propulsion for Space (HyPr Space)

    France

    135

    advancing thermal management: heat flow analysis and hotspot identification in solid rocket motors

    10

    Mr. Kushal Chatterjee

    R V College of Engineering, Bengaluru

    India

    136

    Thrust Prediction of Hybrid Rocket Motor Based on Physical Feature Embedding and Residual Learning

    10

    confirmed

    Dr. Weile Xu

    Beihang University (BUAA)

    China

    137

    Statistical Thermodynamics Approaches for Advancing Chemical Propulsion Systems

    10

    Mr. Ishaan Dutta

    R V College of Engineering, Bengaluru

    India

    138

    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

    139

    numerical combustion model and efficiency study of electrically ignited solid propellants for micro to macro propulsion systems

    10

    confirmed

    Mr. Abishek Shrestha

    Australia

    140

    NUMERICAL AND EXPERIMENTAL ANALYSIS OF NEW PROPELLANT FORMULATIONS FOR HYBRID ROCKETS

    10

    confirmed

    Mr. Abdul Rahman

    Scuola di Ingegneria Aerospaziale "La Sapienza"

    Italy

    141

    machine learning-based study on thrust prediction of hydrogen peroxide and polyethylene hybrid rocket motor

    10

    withdrawn

    Mrs. Keren Lin

    Beihang University (BUAA)

    China

    142

    H2O2/HDPE Hybrid Rocket: Experimental and Theoretical Investigation

    10

    confirmed

    Mr. Abdul Rahman

    Scuola di Ingegneria Aerospaziale "La Sapienza"

    Italy

    143

    Development of Carbon Fiber Rocket Motors with Insulative Laminate Structure

    10

    Mr. Ishaan Dutta

    R V College of Engineering, Bengaluru

    India

    144

    AI and Classical Approaches to Estimating Solid Fuel Regression Rate in Hybrid Rocket Engines

    10

    confirmed

    Mr. Gabriel Metre Resende

    University of Brasilia

    Brazil