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  • 7
  • 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

    2012-10-04

    Time

    15:15

    Room

    TS07 (Sala Regulus, Hall 3)

    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

    Recent Thermal Design Driven Development Activities at MT Aerospace

    15'

    confirmed

    Dr. Farid Infed

    MT Aerospace AG

    Germany

    2

    Cryogenics tasks in perspective Russian scientific space projects

    15'

    confirmed

    Mr. Anton Burdanov

    Central Research Institute for Machine Building (JSC TSNIIMASH)

    Russian Federation

    3

    Coating effects on thermal properties of carbon carbon and carbon silicon carbide composites for space thermal protection systems.

    15'

    confirmed

    Dr. Marta Albano

    Sapienza University of Rome

    Italy

    4

    Chemical non equilibrium simulations of hypersonic flights in carbon dioxide-nitrogen atmospheres using a coupled Euler-second-order boundary layer method

    15'

    withdrawn

    Mr. Martin Starkloff

    University of the Federal Armed Forces Munich

    Germany

    5

    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    withdrawn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

    6

    EXPERT – The ESA Experimental Re-Entry Vehicle: Experiments and Payloads qualified and ready for the flight

    15'

    confirmed

    Dr. Antonio Del Vecchio

    CIRA Italian Aerospace Research Centre

    Italy

    7

    Large Scientific Satellite Tested with Success at LIT-INPE 6m x 8m Space Simulation Chamber

    15'

    confirmed

    Dr. Jose Sergio Almeida

    Instituto Nacional de Pesquisas Espaciais (INPE)

    Brazil

    8

    Uncertainty quantification for hypersonic flow simulations

    15'

    withdrawn

    Mr. Jeroen Cappaert

    International Space University (ISU)

    France

    9

    Effect of Eccentricity on the Heat Transfer Rates of a Re Entry Vehicle with Concave Windward Surface

    15'

    confirmed

    Mr. Gurunadh Velidi

    University of Petroleum and Energy Studies

    India

    10

    Solid rocket booster segment joint - a parametric study

    15'

    withdrawn

    Mr. SHITIJ ARORA

    Vikram Sarabhai Space Centre (VSSC)

    India

    11

    Aerothermodynamics of a Hemispherical-Cylindrical Blunt Vehicle with a Flow through Duct

    15'

    confirmed

    Mr. Gurunadh Velidi

    University of Petroleum and Energy Studies

    India

    12

    Robust neural network control of space robot system with flexible joints

    15'

    no-show

    Dr. Zhiyong Chen

    China

    13

    Effect of forebody configuration on nonslender delta wing rock

    Poster

    withdrawn

    Mr. Bing Han

    College of Astronautics, Northwestern Polytechnical University

    China

    14

    Computational analysis of thermal and structural loads on re-entry vehicles and a conceptual SSTO model using an in-house solver code.

    Poster

    withdrawn

    Mr. Shrrirup Nambiar

    DEFENCE INSTITUTE OF ADVANCED TECHNOLOGY

    India

    15

    Numerical analysis of engine cylinder liner with inner functionally graded thermal barrier coating

    Poster

    Mrs. Lihong Yang

    Harbin Engineering University

    China

    16

    The Hungarian CoCoRAD experiment in the BEXUS program of the ESA

    Poster

    confirmed

    Mr. Balazs Zabori

    Budapest University of Technology and Economics

    Hungary

    17

    Aeroheating and Structure Coupled Analysis in Thermal Protection System for Reusable Launch Vehicle

    Poster

    confirmed

    Mr. Shiyong Huang

    China Academy of Launch Vehicle Technology (CALT)

    China

    18

    Analysis of load transmission line on the fuselage of reusable launch vehicle

    Poster

    confirmed

    Mrs. Ma Tingting

    China Academy of Launch Vehicle Technology (CALT)

    China

    19

    Simulation of multi-body separation of aerospace vehicles based on unstructured overset grids technology

    Poster

    confirmed

    Mr. Zhou Liu

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    20

    Correction of Hypersonic Viscous Interaction Correlation Parameter

    Poster

    confirmed

    Mr. Gong Anlong

    China

    21

    An all-speed unstructuredflow solver for separation process

    Poster

    confirmed

    Mr. YueLong He

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    22

    Numerical simulation of uav carrier-landing interactive flowfield

    Poster

    confirmed

    Mr. YueLong He

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    23

    Numerical simulation of aerodynamic heating on hypersonic slip flow

    Poster

    confirmed

    Mr. Guo-hao DING

    National University of Defense Technology

    China

    24

    Modeling of hydrogen embrittlement at steady state at high temperature using a commercial finite element program

    Poster

    withdrawn

    Dr. Wissam Bouajila

    DLR, German Aerospace Center

    Germany

    25

    Acoustic-elastic of flight vehicle

    Poster

    Mr. pei xi

    Northwestern Polytechnical University

    China

    26

    Investigate of rudder deflected multi-body separation

    Poster

    confirmed

    Dr. Dun Li

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    Aerothermal Analysis of Ultra High Temperature Ceramics Flying Test Bed

    with 14761

    Dr. Mario De Stefano Fumo

    CIRA Italian Aerospace Research Centre

    Italy