IPB

session IPB

Title: Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM
type: interactive
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
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
SOLID MICROROCKETS FOR LOW THRUST APPLICATIONS	12	confirmed	Dr. Antonella Ingenito	Sapienza University of Rome	Italy
Three Dimensional and Multiphase Simulations of Aft-Finocyl Solid Rocket Motors	12	confirmed	Mr. Gianluca Cocirla	Sapienza University of Rome	Italy
A Methodology and Demonstration for Preliminary Tier Determination Analyses	10	confirmed	Dr. Daniel Clayton		United States
Analysis and Optimization of Nuclear Rocket Options for Crewed Mars Exploration	10	confirmed	Ms. Wu Xunliang	Space Engineering University (Beijing)	China
A Field Reversed Configuration Fusion System Applied to Space Propulsion	10	confirmed	Mr. Charles Henrique M. F. Fernandes	Instituto Tecnológico de Aeronáutica (ITA)	Brazil
Application of Micro electric Propulsion System Based on Additive Manufacturing Technology on Micro Satellites	12	confirmed	Dr. Shen Yan	Edrive Space Technology Co., Ltd	China
HEMPT – Electric Propulsion for LEO/MEO Constellations	12	confirmed	Mr. Angelo Genovese	Thales Electron Devices GmbH	Germany
Sub-Scale Demonstration of a Pulsed Fusion Axial Magnetic Nozzle with a Target-Type Thrust Stand	10	confirmed	Dr. Nathan Schilling	self	United States
Iodine as a propellant: 5 years of successful use in space	12	confirmed	Dr. Dmytro Rafalskyi	ThrustMe	France
Development of a Novel CubeSat-scale Air-breathing Electric Propulsion System	12	confirmed	Dr. Vittorio Giannetti	Scuola Superiore Sant'Anna	Italy
Reactive Molecular Dynamics Simulation of Ammonium Perchlorate-Aluminum Interactions: Effects of Passivation and Initial Decomposition Mechanism	11	confirmed	Prof. Rene Gonçalves	Aeronautic Institute of Technology (ITA)	Brazil
Hybrid Rocket Engine Nozzle Deformation using a Level Set Method	11	confirmed	Mr. Jan Erik Zeriadtke	DLR (German Aerospace Center)	Germany
Development of H3 RCS (Reaction Control System)	12		Mr. yoshihiro kishino	IHI Aerospace Co, Ltd.	Japan
effect of the electrode shape on the combustion characteristics of electrically controlled solid propellant	12	confirmed	Mr. Myoungjin Kim	Chosun University	Korea, Republic of
Design of an Additively Manufactured Bipropellant Thruster for In-Orbit Satellite Operations	12	confirmed	Mr. Michele Ianniello	Politecnico di Milano	Italy
Numerical study of an additively manufactured hybrid rocket engine of 1 kN: A CFD Approach	12	confirmed	Dr. Olexiy Shynkarenko	University of Brasilia	Brazil
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
On-orbit demonstration of RUDRA 0.3 HPGP Green Monopropellant thruster system in POEM-3 PSLV C-58 mission.	12	confirmed	Mr. Saagar Malaichamy	Bellatrix Aerospace Private Limited	India
Highly Throttleable Propulsion for FROG-H: A Green Technological Leap	12	confirmed	Mr. Błażej Marciniak	Łukasiewicz Research Network – Institute of Aviation (ILOT)	Poland
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
Thermo structural assessment of Un-submerged Flex Nozzle system (USFN) with 4-D Carbon- Carbon Nozzle liner	10	confirmed	Mr. Paul Murugan J	Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram	India
EXPLORING THE PERFORMANCE OF INNOVATIVE SOLID FUEL RAMJETS	12	confirmed	Mr. Abdul Rahman	Scuola di Ingegneria Aerospaziale "La Sapienza"	Italy
Blockage Removal and Requalification of a Regeneratively Cooled, Additively Manufactured Rocket Engine	12	confirmed	Mr. Sebastian Bouckenooghe	University of Southern California	United States
Enhancing Bipropellant Attitude Control Thruster Testing: A Control Theory Approach	12	confirmed	Mr. Lars Osborne		United States
Study on Ignition and Combustion Characteristics of Gaseous Oxygen/Gaseous Methane Igniter	12	confirmed	Dr. Yang Zhang	Jiangsu University	China
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
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
Experimental investigations into the low toxicity hypergolic ionic liquid-ethanol fuel and hydrogen peroxide oxidizer	12	confirmed	Dr. Vikas Bhosale	Space Solutions Co. LTD	Korea, Republic of

session IPB

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