IAF Digital Library

4

session 4

Title: Solid and Hybrid Propulsion (2)
type: oral
Description: This session includes all science and technologies supporting all aspects of solid and hybrid propulsion.

IPC members

Co-Chair: Mr. Jerome Breteau, European Space Agency (ESA), France;
Co-Chair: Prof.Dr. Arif Karabeyoglu, Koc University, Türkiye;
Rapporteur: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;
Rapporteur: Dr. Ashley Karp, Jet Propulsion Laboratory - California Institute of Technology, United States;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		A Novel Coordinated Energetic Compound Leading a Promising Concept of Propellant Formula Designing	10	confirmed	Mr. Zhenhao Mi	The 41st Institute of the Fourth Academy, China Aerospace Science and Technology Corporation (CASC)	China
2		Energetic hybrid rocket propellants for upper stage propulsion	10	confirmed	Mr. Vinayak Malhotra	SRM University Chennai	India
3		Performance evaluation of modified loose flap venting scheme introduced for the propellant processing of upper stage SRM through hot test	10	confirmed	Mr. Shubham Maurya	Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram	India
5		Development of a Thrust Control System for Rocket Engines	10	confirmed	Dr. Olexiy Shynkarenko	University of Brasilia	Brazil
6		Experimental and Numerical Study on Feasibility of 5kN Thrust Level Hybrid Rocket Motor using the Low-Melting-Point Thermoplastic Fuel	10	confirmed	Dr. Yo Kawabata		Japan
7		numerical and experimental research on ablation performance of a carbon/carbon composties solid rocket motor nozzle insert	10	confirmed	Dr. Lin Sun	Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory, Northwestern Polytechnical University	China
11		Study on thermoacoustic oscillation characteristics of carbon nanotubes	10	confirmed	Mr. Yu Liao	Northwestern Polytechnical University	China
13		Experimental investigation of a flow-oriented throttleable injector designed for throttleable hybrid rocket motor	10	confirmed	Mr. Zeng Zhao	School of Astronautics, Beihang University	China