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  • session 7

    Title

    Space Vehicles – Mechanical/Thermal/Fluidic Systems

    type

    oral

    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

    2011-10-06

    Time

    15:00

    Room

    TS-17

    IPC members
    • Chairman: Dr. Brij Agrawal, Naval Postgraduate School, United States;

    • Chairman: Prof.Dr. Oleg Alifanov, MAI, Russian Federation;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    A new methodology for estimating surface heat flux from in-depth sensors

    15

    confirmed

    Dr. Jay Frankel

    University of Tennessee

    United States

    2

    Carbon/carbon comparative optimization method for hot structures applications in re-entry environment conditions

    15

    confirmed

    Dr. Marta Albano

    Sapienza University of Rome

    Italy

    3

    Active thermal control system for perspective venusian lander

    15

    confirmed

    Mr. Anton Burdanov

    Central Research Institute for Machine Building (FGUP TSNIIMASH)

    Russian Federation

    4

    A Thermal Model for Analysis and Control of Drilling in Icy Formations on Mars

    15

    confirmed

    Mr. Timothy Szwarc

    Stanford University

    United States

    5

    Egse in spacecraft thermal vacuum tests for accurate power measurements and minimization of power supplies

    15

    confirmed

    Dr. Durval Zandonadi Jr.

    Instituto Nacional de Pesquisas Espaciais (INPE)

    Brazil

    6

    Application of inertia relief in structural strength analysis of reusable launch vehicle

    15

    withdrawn

    Mrs. Ma Tingting

    China Academy of Launch Vehicle Technology (CALT)

    China

    7

    RE-USE OF EXOMARS ROVER ON ICY MOONS OF JUPITER

    15

    withdrawn

    Mr. Abrar-Ul-Haq Khan Baluch

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    8

    Versions of orbiters’ flight systems for nonnuclear action on asteroid Apophis

    15

    confirmed

    Dr. Mykola M. Slyunyaev

    Yuzhnoye State Design Office

    Ukraine

    9

    Spacecraft Aerodynamics and Heat Shield Characteristics Impact on Optimal Aeroassisted Coplanar Orbital Transfer

    15

    confirmed

    Dr. Antonio Mazzaracchio

    Sapienza Università di Roma

    Italy

    10

    Thermal buckling of simply supported moderately thick functionally graded plates

    15

    confirmed

    Ms. Yang Lihong

    China

    11

    Research on Flight experiment Technique to Verification Thermal Protection Materials and Insulation Materials

    15

    withdrawn

    Dr. Yu Yubin

    China Academy of Launch Vehicle Technology (CALT)

    China

    12

    Application of Structured Singular Value Method to Aeroservoelastic Robustic Stability Analysis for Reusable Launch Vehicle

    15

    no-show

    Mr. Junpeng Hui

    China Academy of Launch Vehicle Technology (CALT)

    China

    13

    Flow-Structure-Thermal Investigation of Blunt Body in High-Enthalpy Flows

    15

    no-show

    Mr. Jing Yang

    College of Aerospace and Materials Engineering, National University of Defense Technology

    China