session IPB
- Title
Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM
- Room
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | 12 | Dr. Antonella Ingenito | Sapienza University of Rome | Italy | |||
2 | Three Dimensional and Multiphase Simulations of Aft-Finocyl Solid Rocket Motors | 12 | confirmed | Mr. Gianluca Cocirla | Sapienza University of Rome | Italy | |
3 | A Methodology and Demonstration for Preliminary Tier Determination Analyses | 10 | confirmed | Dr. Daniel Clayton | United States | ||
4 | Analysis and Optimization of Nuclear Rocket Options for Crewed Mars Exploration | 10 | confirmed | Ms. Wu Xunliang | Space Engineering University (Beijing) | China | |
5 | A Field Reversed Configuration Fusion System Applied to Space Propulsion | 10 | confirmed | Mr. Charles Henrique M. F. Fernandes | Instituto Tecnológico de Aeronáutica (ITA) | Brazil | |
6 | 12 | confirmed | Dr. Shen Yan | Edrive Space Technology Co., Ltd | China | ||
7 | 12 | confirmed | Mr. Angelo Genovese | Thales Electron Devices GmbH | Germany | ||
8 | Sub-Scale Demonstration of a Pulsed Fusion Axial Magnetic Nozzle with a Target-Type Thrust Stand | 10 | confirmed | Dr. Nathan Schilling | self | United States | |
9 | 12 | Dr. Dmytro Rafalskyi | ThrustMe | France | |||
10 | Development of a Novel CubeSat-scale Air-breathing Electric Propulsion System | 12 | confirmed | Dr. Vittorio Giannetti | Scuola Superiore Sant'Anna | Italy | |
11 | 11 | confirmed | Prof. Rene Gonçalves | Aeronautic Institute of Technology (ITA) | Brazil | ||
12 | Hybrid Rocket Engine Nozzle Deformation using a Level Set Method | 11 | confirmed | Mr. Jan Erik Zeriadtke | DLR (German Aerospace Center) | Germany | |
13 | 12 | Mr. yoshihiro kishino | IHI Aerospace Co, Ltd. | Japan | |||
14 | 12 | confirmed | Mr. Myoungjin Kim | Chosun University | Korea, Republic of | ||
15 | Design of an Additively Manufactured Bipropellant Thruster for In-Orbit Satellite Operations | 12 | confirmed | Mr. Davide Zuin | Politecnico di Milano | Italy | |
16 | Numerical study of an additively manufactured hybrid rocket engine of 1 kN: A CFD Approach | 12 | confirmed | Dr. Olexiy Shynkarenko | University of Brasilia | Brazil | |
17 | Preliminary design of a throttleable hybrid rocket engine using the A-SOFT principle | 12 | confirmed | Mr. Joël Martin | Deutsch Luft und Raumfahrt Zentrum (DLR) | Germany | |
18 | 12 | confirmed | Mr. Saagar Malaichamy | Bellatrix Aerospace Private Limited | India | ||
19 | Highly Throttleable Propulsion for FROG-H: A Green Technological Leap | 12 | confirmed | Mr. Błażej Marciniak | Łukasiewicz Research Network – Institute of Aviation (ILOT) | Poland | |
20 | A SMALL LAUNCHER INCLUDING A DUAL MODE RAMJET AS SECOND STAGE | 12 | confirmed | Mr. Lakshmi Narayana Phaneendra Peri | Scuola di Ingegneria Aerospaziale "La Sapienza" | Italy | |
21 | 10 | confirmed | Mr. Paul Murugan J | Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram | India | ||
22 | 12 | Mrs. Sai Gowthimi Kaluguru | RMIT University (Royal Melbourne Institute of Technology) | Australia | |||
23 | 12 | confirmed | Mr. Sebastian Bouckenooghe | University of Southern California | United States | ||
24 | Enhancing Bipropellant Attitude Control Thruster Testing: A Control Theory Approach | 12 | confirmed | Mr. Lars Osborne | United States | ||
25 | Study on Ignition and Combustion Characteristics of Gaseous Oxygen/Gaseous Methane Igniter | 12 | confirmed | Dr. Yang Zhang | Jiangsu University | China | |
26 | Sustainable Spacecraft Propulsion: A 1N Thrust-Level Bi-Propellant Thruster utilizing Nitrous Oxide | 12 | confirmed | Mr. Varun Reddy Nandyala | FOTEC Forschungs- und Technologietransfer GmbH | Austria | |
27 | A numerical optimization of high-altitude test facility for upper stage engines | 12 | confirmed | Dr. chaehyoung kim | Korea Aerospace Research Institute (KARI) | Korea, Republic of | |
28 | 12 | confirmed | Dr. Vikas Bhosale | Space Solutions Co. LTD | Korea, Republic of |