IAF Digital Library

1

session 1

Title: Liquid Propulsion (1)
type: oral
Description: This session is dedicated to all aspects of Liquid Rocket Engines.
Date: 2021-10-25
Time: 15:15
Room: Ajman D

IPC members

Co-Chair: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;
Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;
Rapporteur: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;
Rapporteur: Mr. Akira Ogawara, Mitsubishi Heavy Industries, Ltd., Japan;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	15:15	Data-driven emulation models for Rocket Engines injector design	15	confirmed	Mr. Jose Felix Zapata Usandivaras	ISAE-Supaero University of Toulouse	France
2	15:30	Design of a conical anti-slosh baffle and its experimental validation for slosh stability for the Indian interplanetary mission	15	confirmed	Mr. Sarath Chandran Nair S	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
4	15:45	Preliminary Test of Hydrogen Peroxide Thermal Decomposition Monopropellant Thruster	15	confirmed	Mr. Seungho Lee	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
6	16:00	Development of an additively manufactured Hydrogen Peroxide / Kerosene 6 kN aerospike breadboard engine	15	confirmed	Mr. Tim Dorau	TU Dresden	Germany
8	16:15	Liquid Upper Stage Demonstrator Engine (LUMEN): Overview and Project Progress	15	confirmed	Mr. Tobias Traudt	DLR (German Aerospace Center)	Germany
11	16:30	comparison between a 400n electric pump fed hydrogen peroxide/ethanol thruster and the mmh/nto legacy systems	15	confirmed	Ms. Livia Ordonez Valles	Hochschule Bremen	Germany
1003	16:45	The results of ground development tests of the RD861K high-altitude liquid-propellant restartable rocket engine	15	confirmed	Mr. Yevgen Strelchenko	Yuzhnoye State Design Office	Ukraine
1005	17:00	Ariane 6 Upper Liquid Propulsive Module Qualification	15	confirmed	Mr. Patrick Danous	ArianeGroup	France
1007	17:15	Experimental characterization and analysis of passive flow separation control of upper stage rocket nozzle during sea-level testing	15	confirmed	Dr. Ganesh Paramasivan	ISRO Propulsion Complex, Mahendragiri, India	India
1009	17:30	Tests to study the influence of the low temperature of structure and propellants on the performance of VEGA Stage 4 main engine	15	confirmed	Mr. Andrii Kovalenko	Yuzhnoye State Design Office	Ukraine
1010	17:45	Combined pressurization system and gas-reactive control system of the reusable stage of the launch vehicle	15	withdrawn	Mr. Vladislav Urbansky	Omsk State Technical University	Russian Federation
1012	18:00	Experimental & Numerical Investigation of GOX/GCH4 Combustion in 7- Element Sub-scale Combustor	15	confirmed	Mr. Abhishek Sharma	Indian Space Research Organization (ISRO)	India