• Home
  • IAF Digital Library
  • Public Website
  • My papers
  • Home
  • event
  • IAC-21
  • C4
  • 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    withdrawn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    withdrawn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    withdrawn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