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  • session 1

    Title

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

    type

    oral

    Description

    The topics to be addressed include evaluation of analysis versus test results, spacecraft and launch vehicles system and subsystems, e.g. pressurised structures, tanks, loads introduction, primary structures, fluidic equipment, control surfaces; examination of both on-ground and in-orbit testing, launch dynamic environment as related to structural design, space vehicles development and launch verification such as sine, random and acoustic vibration testing and lessons learned.

    Date

    2016-09-26

    Time

    15:15

    Room

    Salon de Eventos 1

    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

    Semi-analytical methods for rapid pre-dimensioning of launcher structures subjected to Booster load introduction

    15'

    confirmed

    Prof.Dr. Andreas Rittweger

    DLR (German Aerospace Center)

    Germany

    2

    the development status of the structure subsystem for enhanced epsilon launch vehicle

    15'

    confirmed

    Mr. Hiroshi Ikaida

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    3

    the failure mode analysis of the 1/20 end frame of the interstage section

    15'

    withdrawn

    Mrs. Shengnan Wang

    China Academy of Launch Vehicle Technology (CALT)

    China

    4

    Structural Design, Analysis and Testing of Launch Vehicle Interface for Small Satellite, Pratham, IIT Bombay

    15'

    confirmed

    Mr. Sumit Jain

    Indian Institute of Technology

    India

    5

    Structural- and Thermomechanical Analyses of Adhesively Bonded Joints for Modular Satellite Structures

    15'

    withdrawn

    Mr. Thomas A. Schervan

    RWTH Aachen University

    Germany

    6

    ultralight PBO composite overwrapped pressure vessels for Change’s 5 detector

    15'

    Dr. Fei Yan

    Shanghai Institute of Space Propulsion

    China

    7

    cryogenic properties of carbon fiber reinforced composites support structure

    15'

    confirmed

    Ms. Hongfei Zheng

    China

    8

    Numerical Simulation and Analysis for Point Separating Pyroshock Source and the Load Forming Mechanism of the Interface of Spacecraft and Launch vehicle

    15'

    withdrawn

    Mrs. Xin Zhao

    Institute of Spacecraft System Engineering,China Academy of Space Technology (CAST)

    China

    9

    Design, Verification and Ground Qualification Approach for the Structure of the European Service Module of the Orion Multi-Purpose Crew Vehicle

    15'

    confirmed

    Dr. Gandolfo Di Vita

    ESA

    The Netherlands

    10

    Cubesat System structural Design

    15'

    confirmed

    Dr. Barbara Bermudez-Reyes

    Universidad Autonoma de Nuevo Leon

    Mexico

    11

    Characterization of spring stiffness variation of solid rocket motor flex seals due to combustion chamber pressure

    15'

    confirmed

    Mr. Arun Krishnan

    Indian Space Research Organization (ISRO)

    India

    12

    plastic zone at the mixed mode crack tip in nickel-based single crystal plate based on a modified yield criterion

    15'

    withdrawn

    Ms. lihong yang

    Harbin Engineering University

    China

    13

    an overview of experimental and numerical efforts on supercritical injection and combustion for liquid rocket engines

    15'

    confirmed

    Dr. Yuanqi Li

    Xian Aerospace Propulsion Institute

    China