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  • session 7

    Title

    Space Vehicles – Mechanical/Thermal/Fluidic Systems

    Description

    The topics to be addressed include novel technical concepts for mechanical/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.

    Date

    2013-09-26

    Time

    14:45

    Room

    306B

    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

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    15'

    Parametric Shape Optimization of Reentry Module for Space Missions

    Dr. Ugur Guven

    United States

    2

    confirmed

    15'

    Thermal modeling of the adaptive thermal control microsystem of the spacecraft

    Mr. Anatoliy Patsievskiy

    S.P. Korolev Rocket and Space Corporation Energia

    Russian Federation

    3

    confirmed

    15'

    Global error estimation in CFD mesh coarsening process for uncertainty quantification methods

    Mr. Martin Kubicek

    University of Strathclyde

    United Kingdom

    4

    confirmed

    15'

    Cooling system for high energy potential space vehicle

    Mr. Anton Burdanov

    Central Research Institute for Machine Building (FGUP TSNIIMASH)

    Russian Federation

    5

    withdrawn

    15'

    Heat Transfer Management by Aerospikes for a Hypothesized Lifting Body in Hypersonic Flow

    Dr. Shashank Khurana

    The University of TOKYO, Graduate school

    China

    6

    confirmed

    10'

    aerodynamic improvement of the brazilian satellite launch vehicle

    Mr. Col. Jose Duarte

    Instituto de Aeronáutica e Espaço (IAE)

    Brazil

    7

    confirmed

    10'

    Numerical study of active cooling techniques of a nano satellite using CFD for performance enhancement

    Mr. Mollik Nayyar

    Manipal Institute of Technology, Manipal University

    India

    8

    confirmed

    10'

    Aerodynamic Design of a Capsule Configuration for High-speed Manned Re-entry

    Mr. Bingyan Chen

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    9

    confirmed

    10'

    variable inertia fluidic ring actuator on attitude control and residual fuel management systems

    Ms. Hong Guan

    Beihang University

    China

    10

    confirmed

    10'

    the study on iot based manufacturing system for astronautical products

    Mr. Xie Xinping

    Nanjing University of Aeronautics and Astronautics

    China

    11

    confirmed

    10'

    Thermal Mapping and Trends of Mars Analog Materials in Sample Acquisition Operations Using Experimentation and Models

    Mr. Timothy Szwarc

    Stanford University

    United States

    12

    confirmed

    10'

    Transient study about the heat transfer of sublimator combined with fluid loop

    Dr. Yuying WANG

    Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology

    China

    13

    confirmed

    10'

    Materials surface emissivity analyses performed by the combined use of dual and single color optical pyrometers

    Dr. Carlo Purpura

    CIRA Italian Aerospace Research Centre

    Italy