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: 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	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3	the failure mode analysis of the 1/20 end frame of the interstage section	15'	withdrawn	Mrs.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5	Structural- and Thermomechanical Analyses of Adhesively Bonded Joints for Modular Satellite Structures	15'	withdrawn	Mr.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Point Separating Pyroshock Source and the Load Forming Mechanism of the Interface of Spacecraft and Launch vehicle	15'	withdrawn	Mrs.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

session 1

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