IAF Digital Library

2

session 2

Title: Propulsion System (2)
Description: This session is dedicated to all aspects of Solid and Hybrid Propulsion.
Date: 2019-10-23
Time: 09:45
Room: 143A

IPC members

Co-Chair: Mr. Stéphane Henry, France;
Co-Chair: Dr. Toru Shimada, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency, Japan;
Rapporteur: Dr. Yen-Sen Chen, American Institute of Aeronautics and Astronautics (AIAA), United States;
Rapporteur: Dr. Mario Kobald, German Aerospace Center (DLR), Germany;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	09:45	KEYNOTE: OmegA Launch Vehicle	25	confirmed	Mr. Kent Rominger	Northrop Grumman Innovation Systems	United States
2	10:10	Ariane 6 and Vega-C programs: the P120C SRM nozzle qualification	13	confirmed	Mr. ERIC GAUTRONNEAU	ArianeGroup SAS	France
3	10:23	Performance evaluation of 4D Carbon-Carbon throat insert through Hot test of Solid Motor	13	confirmed	Mr. Siva kumar Ganesan	Indian Space Research Organization (ISRO)	India
4	10:36	Design and Developmental Challenges of Slow Burning Solid Booster for Sub-orbital Hyper Sonic re-entry Experiment	13	no-show	Dr. ACHUTANANDA PARHI	Indian Space Research Organization (ISRO)	India
5	10:49	Performance and environmental impact prediction of SRMs. Road map for reliable dataset of particles in plume	13	confirmed	Ms. Stefania Carlotti	Politecnico di Milano	Italy
6	11:02	Analysis of Solid Propellant Combustion Using Image Processing Techniques	13	confirmed	Ms. Sonali Sinha Roy	Purdue University	United States
7	11:15	Mars Ascent Vehicle (MAV) Preliminary Architecture Assessment Overview	13	confirmed	Ms. Angie Jackman	NASA	United States
8	11:28	A Study on New Hybrid Rocket Engine with Multi-Section Swirl Injection and Aft Counter-Swirl Injection Method	13	confirmed	Prof. Shigeru Aso	Kyushu University	Japan
9	11:41	Real-time regression rate measurement of an additive-manufactured functional hybrid rocket fuel	13	confirmed	Dr. Kohei Ozawa	Kyushu Institute of Technology	Japan
10	11:54	Cost-Effective Hybrid Rocket Launch Vehicle of Taiwan	13	confirmed	Dr. Yen-Sen Chen	American Institute of Aeronautics and Astronautics (AIAA)	United States
11	12:07	Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-based Formulations	13	confirmed	Mr. Riccardo Bisin	Politecnico di Milano	Italy
12	12:20	dynamic response of thrust modulation in hybrid rocket for VTVL propulsion system	13	confirmed	Prof. Changjin Lee	Konkuk University	Korea, Republic of
13	12:33	Performance Analysis of N2O/CO2 Oxidizer Mixture with Paraffin based Micro-Aluminum Fuel for Mars Ascent Vehicles	13	confirmed	Mr. Ozan Kara	Space Generation Advisory Council (SGAC)	Türkiye
*		Hybrid Propulsion: Innovative Formulations Based on Paraffin / Ethanol Interaction			Prof.Dr. Rene Gonçalves	Instituto Tecnológico de Aeronáutica (ITA)	Brazil
*		impact assessment of propellant entrapment in loose flap cavity on ballistic performance and validation through hot test of solid rocket booster		withdrawn	Mr. Arun Raj	Vikram Sarabhai Space Centre (VSSC)	India