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  • session 2

    Title

    Liquid Propulsion (2)

    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.

    IPC members
    • Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;

    • Co-Chair: Mr. Didier Boury, ArianeGroup SAS, France;

    • Rapporteur: Prof. Changjin Lee, Konkuk University, Korea, Republic of;

    • Rapporteur: Mr. Martin Velander, GKN Aerospace Engine Systems, Sweden;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Spray Angle Evolution of Flash Boiling Liquid Nitrogen Sprays During the Start-up of High-Altitude Liquid Rocket Engines

    15

    withdrawn

    Mr. Andreas Rees

    DLR (German Aerospace Center)

    Germany

    2

    Design & Development of Propellant Intake Device for Cryo Upper Stage LOX Tank

    15

    confirmed

    Mr. Aamir Yusuf

    Liquid Propulsion System centre

    India

    3

    Numerical analysis of LE-9 engine turbopumps

    15

    withdrawn

    Dr. Satoshi Ukai

    JAXA

    Japan

    4

    Investigation on flow-type coupling oscillations of the preburner sub-system of the staged combustion cycle engine

    15

    Dr. Yuanqi Li

    Science and Technology on Liquid Rocket Engine Laboratory, Xi’an Aerospace Propulsion Institute

    China

    5

    hot-firing test under high altitude simulated conditions and sea level conditions of the 7-tonf-class engine for KSLV-II

    15

    withdrawn

    Dr. Kwang-Jin Lee

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    6

    heat transfer and pyrolysis characteristics of methane in rocket nozzle cooling channels

    15

    confirmed

    Mr. Jules Heldens

    KTH Royal Institute of Technology

    Sweden

    7

    Numerical Investigation of Subcritical Combustion in Cryogenic Rocket Engine

    15

    confirmed

    Mr. Abhishek Sharma

    Indian Space Research Organization (ISRO)

    India

    8

    photographic investigation of impinging combustion for the hydrogen peroxide and amine-based hypergolic propellant

    15

    confirmed

    Mr. Kyu-Seop Kim

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    9

    Design and development of a large stroke and high cyclic life solenoid valve for bi-propellant spacecraft thrusters

    15

    confirmed

    Mr. Venkata Sunil Sai Nukala

    Indian Space Research Organization (ISRO)

    India

    10

    Computational Fluid Dynamics Model for an Additively Manufactured Liquid Bi-Propellant Coaxial Swirl Injector

    15

    Mr. Nathan Radomski

    The Ohio State University College of Engineering

    United States

    11

    ACTiVE use of side forces on aerospike nozzles

    15

    Mr. Martin Propst

    TU Dresden

    Germany

    12

    Hydraulic Model 3 Test Campaign for Verification of the Bang-Bang Pressurization System of the Orion European Service Module

    15

    confirmed

    Mr. Markus Jaeger

    Airbus Defence & Space, Space Systems

    Germany

    13

    effect of floating ring seal clearance on the performance of centrifugal pump used in liquid rocket engine

    confirmed

    Mr. Kiran Rajendran

    Liquid Propulsion Systems Centre(LPSC), Indian Space Research Organization (ISRO)

    India

    14

    development status of additive manufacturing components for le-9 engine

    Mr. Masaki Adachi

    Mitsubishi Heavy Industries, Ltd.

    Japan

    15

    Efficiency of high-temperature generator pressurization systems of liquid methane LV tanks

    confirmed

    Mr. Roman Petrenko

    Yuzhnoye State Design Office

    Ukraine