IAF Digital Library

2

session 2

Title: Liquid Propulsion (2)
type: oral
Description: This session includes all science and technologies supporting all aspects of liquid propulsion. The emphasis in this session is placed, in particular, on components for liquid propulsion.
Date: 2021-10-27
Time: 09:45
Room: Ajman D

IPC members

Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;
Co-Chair: Mr. Didier Boury, ArianeGroup SAS, France;
Rapporteur: Mr. Martin Velander, GKN Aerospace Engine Systems, Sweden;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
8	09:45	ACTiVE USE OF SIDE FORCES ON AEROSPIKE NOZZLES	12	confirmed	Mr. Martin Propst	TU Dresden	Germany
9	09:57	Reactive molecular dynamics of alternative fuels for liquid propulsion systems	12	confirmed	Prof.Dr. Rene Gonçalves	Instituto Tecnológico de Aeronáutica (ITA)	Brazil
14	10:09	Development and coupled Thruster / Electrolyzer Tests of a Water Propulsion System	12	confirmed	Mr. Ulrich Gotzig	ArianeGroup	Germany
1001	10:21	Development of 500N class bipropellant ceramic thruster for SLIM(Smart Lander for Investigating Moon)	13	confirmed	Mr. Daijiro Shiraiwa	MHI	Japan
1002	10:34	ispace’s Low-Cost Lunar Lander Propulsion System a Design Overview	12	withdrawn	Mr. Alex Konietzke	ispace, inc.	Japan
1003	10:46	Catalytic combustion in a reactor with an alternative HEHN monopropellant	12	withdrawn	Mr. Ju Won Kim	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
1004	10:58	off-design hypergolic combustion of the high test peroxide-based propellant	12	withdrawn	Mr. Kyu-Seop Kim	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
1005	11:10	Low-Order Dynamic Model of Hydrogen Peroxide Catalytic Reactor for Transient Behavior Prediction	12	confirmed	Mr. Sukmin Choi	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
1006	11:22	Large Eddy Simulation of Self-Excited Combustion Instability in a Continuously Variable Resonant Combustor	12	confirmed	Mr. Sarath Chandran Nair S	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
1007	11:34	Numerical and experimental investigation of Lambda type seals in high-pressure cryogenic bolted joints	12	confirmed	Mr. Vivek S	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
1010	11:46	Combustion Performance Enhancement of Bi-propellant Thruster Using Fluidic Oscillator Kerosene Injector	12	withdrawn	Mr. Sangwoo Jung	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
1011	11:58	Feasibility of a dual-plate injector for throttling of monopropellant thruster	12	withdrawn	Ms. Yehyun Kim	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
1012	12:10	A parametric blade design study in the Baljé-Diagram: application to supersonic impulse turbines	12	withdrawn	Mr. Robson Hahn	DLR, German Aerospace Center	Germany
1013	12:22	Analysis of pressure fluctuation characteristics of high speed centrifugal pump	12	confirmed	Ms. Naidi Chen	Beijing Aerospace Propulsion Institute	China
*		Cyclic stress analysis of Semicryo engine thrust chamber using Chaboche unified viscoplastic model			Dr. Ahmedul Asraff	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
*		dynamic characteristics of turbopump rotor system for high thrust lox-kerosene engine			Dr. Feiping Du	Xi'an Aerospace Propulsion Institute	China
*		multi-scale numerical study on atomization process of gas-liquid pintle injector for liquid rocket engine			Mr. Pu Shi	Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory, Northwestern Polytechnical University	China