IAF Digital Library

3

session 3

Title: Solid and Hybrid Propulsion (1)
Description: This session is dedicated to all aspects of Solid and Hybrid Rocket motor.
Date: 2021-10-26
Time: 09:45
Room: Ajman D

IPC members

Co-Chair: Mr. Stéphane Henry, France;
Co-Chair: Dr. Mario Kobald, HyImpulse Technologies GmbH, Germany;
Rapporteur: Mr. Jean-Claude Traineau, Office National d’Etudes et de Recherches Aérospatiales (ONERA), France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
2	09:45	BALLISTIC STUDY OF SOLID PROPELLANTS UNDER THE INFLUENCE OF VARYING PERCENTAGES OF IRON OXIDE	13	confirmed	Ms. Aishwarya Alur	R V College of Engineering, Bengaluru	India
5	09:58	Student firing tests and launches with commercial and self-made solid rocket motors	13	confirmed	Dr. Mario Tindaro Migliorino	Sapienza University of Rome	Italy
6	10:11	concept study of chemical micropropulsion system using combustion of micron-sized aluminum particles and water-vapor	13	confirmed	Mr. masaya murohara	The University of TOKYO, Graduate school	Japan
7	10:24	RMD Simulation and Combustion Evaluation of Paraffin/GOx for Hybrid Rocket Motors	13	confirmed	Prof.Dr. Rene Gonçalves	Instituto Tecnológico de Aeronáutica (ITA)	Brazil
8	10:37	reducing plant dynamics change for thrust modulation in hybrid rocket combustion using pid gain scheduling	13	confirmed	Mr. Donghoon Chae	Konkuk University	Korea, Republic of
9	10:50	RAVEN: a student rocket program at Luleå University of Technology, Sweden	13	confirmed	Ms. Kiira Tiensuu	Luleå University of Technology	Sweden
10	11:03	Numerical analysis of a N2O/paraffin fueled hybrid rocket to perform capture maneuvers in a Mars orbit	13	confirmed	Mr. Renato de Brito do Nascimento Filho	Univerisity of Brasilia	Brazil
12	11:16	Reaction Rate Measurement of Wire-Fed Magnesium in Water-Vapor Flow for Micropropulsion System	13	confirmed	Ms. Mariko Akiyama	University of Tokyo	Japan
1001	11:29	KEYNOTE: P120C Solid Rocket Motor Nozzle Development	30	withdrawn	Mr. Yann Talamoni	ArianeGroup	France
1003	11:59	EFFECT OF RESIDUAL STRAIN ON STRUCTURAL INTEGRITY OF SRM GRAIN DURING IGNITION	13	confirmed	Mr. Pu Shi	Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory, Northwestern Polytechnical University	China
1004	12:12	Coupling analysis of temperature and stress in the curing process of SRM's composite case	13	confirmed	Ms. Qun Liang	Northwestern Polytechnical University	China
1011	12:25	Conductive Heat Transfer Effects in Cu-Infused Hybrid Rocket Regression	13	withdrawn	Mr. Kurt Olsen	Utah State University	United States