IAF Digital Library

4

session 4

Title: Solid and Hybrid Propulsion (2)
Description: This session includes all science and technologies supporting all aspects of solid and hybrid propulsion.
Date: 2022-09-20
Time: 10:15
Room: W05

IPC members

Co-Chair: Mr. Didier Boury, ArianeGroup SAS, France;
Co-Chair: Dr. Adam Okninski, Łukasiewicz Research Network – Institute of Aviation (ILOT), Poland;
Rapporteur: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;
Rapporteur: Prof.Dr. Arif Karabeyoglu, Koc University, Türkiye;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	pressure oscillation in p120c srm: what had to be proved	15	confirmed	Mrs. Severine Larrieu	ArianeGroup	France
2	10:30	The Three-Dimensional Combustion Flame of Micron Aluminum Particles Base on Computed Tomography of Chemiluminescence (CTC)	15	confirmed	Dr. Bingning JIN	Northwestern Polytechnical University	China
3	10:45	Study of the influence of the electric field on the incidental ignition of aluminized compound solid propellent via electrostatic discharge	15	confirmed	Prof. Rene Gonçalves	Aeronautic Institute of Technology (ITA)	Brazil
4	11:00	Framework for the design of solid propellants via functionally graded, additively manufactured nanoenergetic materials	15	confirmed	Mr. Connor MacRobbie	University of Waterloo	Canada
5	11:15	Experimental Investigation of Different Propellants and Expandable Graphite Additives for Controlling Rocket Motor Thrust	15	confirmed	Ms. Gabriele Muller	TECHNION - Israel Institute of Technology	Israel
6	11:30	Centrifugal Casting of Paraffin Wax: Numerical Analysis of the Influence of Casting Tube Aspect Ratio	15	confirmed	Prof. Danielle Wood	Massachusetts Institute of Technology (MIT)	United States
7	11:45	Experimental investigation and numerical simulation on throttleable pintle-centrifugal injector for hybrid rocket motor	15	confirmed	Mr. Tianwen Li	School of Astronautics, Beihang University	China
8	12:00	static and re-ignition test of hypergolic hybrid rocket using hydrogen peroxide oxidizer	15	confirmed	Mr. Junyeong Jeong	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
9	12:15	Prediction Of Hybrid Rocket Nozzle Behaviour Under High Temperature Oxygen Rich Environment	15	confirmed	Ms. Sule Ozturk	Deltav Space Technologies,Inc.	Türkiye
10	12:30	Cryogenic Pump Design and Testing for Hybrid Rocket Applications	15	confirmed	Mr. Berkay Terzi	Deltav Space Technologies,Inc.	Türkiye