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  • 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.

    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

    2

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

    10

    confirmed

    Mr. Aamir Yusuf

    Liquid Propulsion System centre

    India

    6

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

    10

    confirmed

    Mr. Jules Heldens

    Royal Institute of Technology (KTH)

    Sweden

    7

    Numerical Investigation of Subcritical Combustion in Cryogenic Rocket Engine

    10

    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

    10

    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

    10

    confirmed

    Mr. Venkata Sunil Sai Nukala

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

    India

    12

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

    10

    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

    10

    confirmed

    Mr. Kiran Rajendran

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

    India

    15

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

    10

    confirmed

    Mr. Roman Petrenko

    Yuzhnoye State Design Office

    Ukraine