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  • session 7

    Title

    Space Vehicles – Mechanical/Robotic/Thermal/Fluidic Systems

    Description

    The topics to be addressed include novel technical concepts for mechanical/robotic/thermal/fluidic systems and subsystems of launchers, manned and unmanned spacecraft, re-entry vehicles and small satellites. Advanced subsystems and design of future exploration missions will be covered, considering issues arising from material selection, cost efficiency and reliability, and advancements in space vehicle development with respect to engineering analysis, manufacturing, and test verification. It is also planned to discuss the issues of experimental and computational simulation of functioning and full-scale tests of space vehicles and their systems / subsystems. Attention will be paid to the problem of verification and validation of mathematical models for the design and experimental development of these objects at various phases of their life cycle.

    Date

    2019-10-24

    Time

    14:45

    Room

    152B

    IPC members
    • Co-Chair: Prof. Oleg Alifanov, Moscow Aviation Institute, Russian Federation;

    • Co-Chair: Dr. Brij Agrawal, Naval Postgraduate School, United States;

    • Rapporteur: Prof. Guoliang Mao, Beijing Institute of Aerodynamics, China;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    14:45

    Boundary Layer Stability and Laminar-Turbulent Transition Analysis with Thermochemical Nonequilibrium Applied to Martian Atmospheric Entry

    12

    confirmed

    Dr. Heather Kline

    National Institute of Aerospace

    United States

    2

    14:57

    INPPS Flagship with iBOSS Building Blocks

    12

    confirmed

    Dr. Frank Jansen

    DLR (German Aerospace Center)

    Germany

    3

    15:09

    Evaluating the Feasibility of Smart Radiator Device (SRD) through Simulated Small Satellite Missions

    12

    confirmed

    Ms. Aimee Carvey

    University of Manitoba

    Canada

    4

    15:21

    Why Did NASA Limit the Use of Magnesium? Flammability and Corrosion Testing of Lightweight Magnesium Alloys for Space Flight Hardware Applications

    12

    confirmed

    Ms. Elizabeth Barrios

    University of Central Florida (UCF)

    United States

    5

    15:33

    Calculating detection of flow’s gas dynamic parameters leap by method of tracking zones.

    12

    Mr. Mikhail Bezpalov

    Harbin Institute of Technology

    China

    6

    15:45

    Diagnostics of defects of thermal protections inflatable re-entry vehicles

    12

    confirmed

    Dr. Alena V. Morzhukhina

    Moscow Aviation Institute (National Research University, MAI)

    Russian Federation

    7

    15:57

    DYNAMIC STALL CHARACTERISTICS OF LOW REYNOLDS NUMBER AIRFOIL IN MARTIAN AND TITAN’S ATMOSPHERE

    12

    confirmed

    Mr. Rajesh Yadav

    University of Petroleum and Energy Studies

    India

    8

    16:09

    thermal design strategy utilizing transformable structure of spacecraft

    12

    confirmed

    Mr. Ryota Ikeda

    Aoyama Gakuin University

    Japan

    9

    16:21

    simulation of rarefied hypersonic flows by using the direct simulation monte carlo method

    12

    confirmed

    Dr. Haiwei Yang

    Harbin Engineering University

    China

    10

    16:33

    Qualification of an Infrared Array Based on NiCr Strips for CBERS 4A Satellite’s Space Simulation Test

    12

    confirmed

    Mr. George Fernandes

    National Institute for Space Research - INPE

    Brazil

    11

    16:45

    RUAG’s development of a modular low-shock jettison system

    12

    confirmed

    Dr. Alberto Sanchez Cebrian

    RUAG Space

    Switzerland

    12

    16:57

    Suitability of Manufacturing Processes for In-Space Manufacturing of Spacecraft Components

    12

    confirmed

    Mr. Matthew Moraguez

    Massachusetts Institute of Technology (MIT)

    United States