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  • session 1

    Title

    Space Structures I - Development and Verification (Space Vehicles and Components)

    Description

    The topics addressed in this session cover the aspects of the development and verification of space vehicle structures (e.g. pressurized propellant tanks, non-pressurized structures of space vehicles, control surfaces) and their components (e.g. fluidic equipment and propulsive lines). The aspects of development, verification and qualification concern: • Thermo-Mechanical loads and environment • New structural concepts (e.g. multi-functional structures, design concepts for reusability) • Structure design and verification (stiffness, strength, static and dynamic stability, damage tolerance, reusability) • Structure optimization • Materials • Static and dynamic ground testing • Exploitation of flight measurements and in-orbit testing • Lessons learned related to space vehicle structures and components development, verification and qualification

    Date

    2019-10-21

    Time

    15:00

    Room

    152B

    IPC members
    • Co-Chair: Mr. Alwin Eisenmann, IABG Industrieanlagen - Betriebsgesellschaft mbH, Germany;

    • Co-Chair: Dr. Andreas Rittweger, DLR (German Aerospace Center), Germany;

    • Rapporteur: Dr. Jochen Albus, ArianeGroup, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:00

    Development & Testing of the Single-Person Spacecraft Crew Enclosure

    12

    confirmed

    Mr. Matthew Stephens

    United States

    2

    15:12

    Verification of a Hypersonic Test Panel through modal analysis of two finite element solvers, and various element types and formulations

    12

    confirmed

    Ms. Erika Lieberknecht

    United States

    3

    15:24

    Fracture Control for Additively Manufactured Spacecraft Structures

    12

    confirmed

    Dr. Mark McElroy

    National Aeronautics and Space Administration (NASA)

    United States

    4

    15:36

    modeling of additive manufactured heat pipes for advanced small satellite design

    12

    confirmed

    Mr. Nikolay Mullin

    Skolkovo Institute of Science and Technology

    Russian Federation

    5

    15:48

    development of H3 launch vehicle 1st stage engine section structure

    12

    confirmed

    Mr. Hiroki Hamajima

    MHI

    Japan

    6

    16:00

    ARIANE 6 UPPER LIQUID PROPULSION MODULE THERMAL PROTECTION HARDWARE DEVELOPMENT AND TESTING

    12'

    confirmed

    Mr. Arturs Jasjukevics

    ArianeGroup

    Germany

    7

    16:12

    Absorptivity Determination Of Satellite Materials from the Transient Heating Phase of a Thermal-Vacuum Test.

    12

    confirmed

    Mr. Khaja Fayaz Hussain

    Scuola di Ingegneria Aerospaziale "La Sapienza"

    Italy

    8

    16:24

    development of large high pressurized xenon tank for electrical propulsion systems

    12

    confirmed

    Dr. Michael Spiegel

    MT Aerospace AG

    Germany

    9

    16:36

    A Condensation Approach for Virtual Shaker Testing Procedures

    12

    confirmed

    Dr. Marcello Remedia

    Surrey Space Centre, University of Surrey

    United Kingdom

    10

    16:48

    Node-Dependent Kinematic Models for the Coupled Load Analysis of Space Structures

    12

    confirmed

    Dr. Enrico Zappino

    Politecnico di Torino

    Italy

    11

    17:00

    A new device and method for simulating hypersonic aerothermal Environment

    12

    confirmed

    Prof.Dr. Dechuan Sun

    School of Aeronautics and Astronautics, Dalian University of Technology

    China

    12

    17:12

    a pseudo method for estimation of elastic plastic burst pressure of cylindrical pressure vessels and its experimental validation.

    12

    confirmed

    Mr. Siva kumar Ganesan

    Indian Space Research Organization (ISRO)

    India