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: 2015-10-12
Time: 15:15
Room: Oranim 1 (ICC, lower level)

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	CRONUS – Sandwich Common Bulkhead Tank Demonstrator	12'	confirmed	Dr. Carina Ludwig	MT Aerospace AG	Germany
2	Assessment on the failure observed in a liquid fuel tank in an aborted mission of a Geosynchronous vehicle	12'	confirmed	Mr. B Kiran Kumar	Indian Space Research Organization (ISRO)	India
3	the equivalent mechanical model for solving spacecraft large amplitude liquid sloshing problem	12'	confirmed	Ms. Shiping Xing	National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an	China
4	A Theoretical Study on the Structural Loads on the Igniter Hardware of Large Solid Boosters and Proof Pressure Testing Adequacy	12'	confirmed	Mr. Yezhil Arasu	Vikram Sarabhai Space Centre (VSSC)	India
5	Design approach adopted for ensuring the structural integrity of a hydraulic line assembly along the Solid Rocket Motor for a Reusable Launch Vehicle technology Demonstration Mission	12'	confirmed	Mr. Thomas Kurian	Indian Space Research Organization (ISRO)	India
6	sizing of the sandwich dominated structure of the gossamer-1 boom and sail deployment unit using ansys solidshell elements	12'	withdrawn	Mr. Johannes Boblenz	Deutsches Zentrum fuer Luft- und Raumfahrt (DLR)	Germany
7	Design, Simulation and Analysis of Carbon-Fiber Composite and Aluminum Honeycomb Rocket Fins Using Fluid-Structure Interaction for Flutter Analysis	12'	confirmed	Mr. Neil Woodcock	Concordia University	Canada
8	Thermal and mechanical design and test campaign results of a single-piece structure for the URSA MAIOR nanosatellite	12'	confirmed	Dr. Lorenzo Arena	University of Rome "La Sapienza"	Italy
9	Thermal environment generation and verification for on-ground testing of launch vehicle’s fairing	12'	no-show	Dr. Lingling CAO	Shanghai Academy of Spaceflight Technology (SAST), China Aerospace and Technology Corporation (CASC)	China
10	Space qualification tests performed by CIRA on the Alta Hall Effect Electric Thruster HT100D	12'	confirmed	Dr. Vito Salvatore	CIRA Italian Aerospace Research Center, Capua	Italy
11	Optimizing 3-Component Force Sensor Installation for Satellite Force Limited Vibration Testing	12'	no-show	Dr. Carmine Salzano		United States
12	Creating a random vibration component test specification for STSAT (Science and Technology Satellite)	12'	no-show	Mr. Talgat Khamitov	JSC «National Company «Kazakhstan Gharysh Sapary»	Kazakhstan

session 1

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