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: 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	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	Ground experimental investigation of thermodynamic vent system for propellant on-orbit storage	12	withdrawn	Mr.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	dual technology strain gauge for on-orbit space structures health monitoring. case report: top see	12	confirmed	Mr. Lorenzo Grossi	Progem	Italy
3	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	Brazilian VLM - Atmospheric stage separation analysis	12	confirmed	Prof. Élcio Jeronimo de Oliveira	Instituto Nacional de Pesquisas Espaciais (INPE)	Brazil
5	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	Optimization of Launcher Liquid Propellant Tanks in CFRP	12	confirmed	Mr. Alexander Schütte	ArianeGroup	Germany
7	Special Testing and Test Strategies for Unique Space Hardware Developments	12	confirmed	Dr. Patric Seefeldt	German Aerospace Center (DLR), Bremen	Germany
8	Assembly and Qualification of a modular satellite structure	12	confirmed	Mr. Thomas A. Schervan	RWTH Aachen University	Germany
9	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	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	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	design of a flight load measurement system for sounding rockets	12	confirmed	Mr. Karl Domjahn	DLR (German Aerospace Center)	Australia
13	Topology Optimization of UokSat3	12	confirmed	Mr. Amr Elhussein	University of Khartoum	Sudan

session 1

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