• Home
  • IAC Papers Archive
  • Public Website
  • My papers
  • Home
  • event
  • IAC-18
  • C2
  • 1
  • session 1

    Title

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

    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

    2018-10-01

    Time

    15:00

    Room

    ÖVB 2

    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

    Ground experimental investigation of thermodynamic vent system for propellant on-orbit storage

    12

    withdrawn

    Mr. Xiaoyu Zhang

    China Academy of Launch Vehicle Technology(CALT)

    China

    2

    15:12

    dual technology strain gauge for on-orbit space structures health monitoring. case report: top see

    12

    confirmed

    Mr. Lorenzo Grossi

    Progem

    Italy

    3

    15:24

    Analytical, Numerical and Experimental Predictions for Free Vibrations and Buckling of Pressurized Orthotropic Cylindrical Shells

    12

    confirmed

    Mr. Felipe Franzoni

    DLR (German Aerospace Center)

    Germany

    4

    15:36

    Brazilian VLM - Atmospheric stage separation analysis

    12

    confirmed

    Prof. Élcio Jeronimo de Oliveira

    Instituto Nacional de Pesquisas Espaciais (INPE)

    Brazil

    5

    15:48

    A systematic approach to the structural design verification for space payloads, lessons learned from Solar Orbiter EPT-HET instrument

    12

    confirmed

    Dr. Ali Ravanbakhsh

    University of Kiel

    Germany

    6

    16:00

    Optimization of Launcher Liquid Propellant Tanks in CFRP

    12

    confirmed

    Mr. Alexander Schütte

    ArianeGroup

    Germany

    7

    16:12

    Special Testing and Test Strategies for Unique Space Hardware Developments

    12

    confirmed

    Dr. Patric Seefeldt

    German Aerospace Center (DLR), Bremen

    Germany

    8

    16:24

    Assembly and Qualification of a modular satellite structure

    12

    confirmed

    Mr. Thomas A. Schervan

    RWTH Aachen University

    Germany

    9

    16:36

    a general framework for aerodynamic thermal test of launch vehicle fairing

    12

    Dr. Lingling CAO

    Shanghai Academy of Spaceflight Technology (SAST), China Aerospace and Technology Corporation (CASC)

    China

    10

    16:48

    Structure Development of the HP3 Instrument Support System for the Mars Mission InSight

    12

    confirmed

    Mr. Tom Sproewitz

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    11

    17:00

    Design optimisation and mass saving of the structure of the ORION-MPCV European Service Module

    12

    confirmed

    Mr. Gandolfo Di Vita

    European Space Agency (ESA)

    The Netherlands

    12

    17:12

    design of a flight load measurement system for sounding rockets

    12

    confirmed

    Mr. Karl Domjahn

    DLR (German Aerospace Center)

    Australia

    13

    17:24

    Topology Optimization of UokSat3

    12

    confirmed

    Mr. Amr Elhussein

    University of Khartoum

    Sudan