session 7

Title: Space Vehicles – Mechanical/Thermal/Fluidic Systems
type: oral
Description: The topics to be addressed include novel technical concepts for mechanical/thermal/fluidic systems and subsystems of launchers, manned and unmanned spacecraft, re-entry vehicles and small satellites. Advanced subsystems and design of future exploration missions will be covered, considering issues arising from material selection, cost efficiency and reliability, and advancements in space vehicle development with respect to engineering analysis, manufacturing, and test verification.
Date: 2017-09-28
Time: 14:45
Room: Panorama Room 2

IPC members

Co-Chair: Dr. Brij Agrawal, Naval Postgraduate School, United States;
Co-Chair: Prof.Dr. Oleg Alifanov, MAI, Russian Federation;
Rapporteur: Prof. Guoliang Mao, Beijing Institute of Aerodynamics, China;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	A novel design approach for space components: application to a multifunctional panel	12	confirmed	Mr. Andrea Emanuele Maria Casini	Politecnico di Torino	Italy
2	thermal optical analysis of LAPAN's IR camera	12	no-show	Mr. Bustanul Arifin	Indonesian Space Agency Secretariat (INASA)	Indonesia
3	The Building Block of Small Space Mechanisms and Robots - A Micro Actuator with High Torque/Weight Ratio	12	confirmed	Dr. Rui Li	Beijing Institute of Control Engineering, China Academy of Space Technology	China
4	Lightweight Means of Actuation for Use in Space-Based Robotics Applications	12	withdrawn	Mr. Scott Brady	University of Strathclyde, Glasgow	United Kingdom
5	Experimental study of Heat Switch Radiator using Shape Memory Alloy for High Insulation System	12	confirmed	Mr. Shunsaku Eguchi	Tokyo University of Science	Japan
6	A STUDY OF ELECTROMAGNETIC ENVIRONMENTAL EFFECTS ON SPACE LAUNCH SYSTEMS BY MEANS OF REVERBERATION CHAMBER	12	confirmed	Dr. Marta Albano	Agenzia Spaziale Italiana (ASI)	Italy
7	Coupled Thermodynamic and Structural Optimization of a Cryogenic Upper Stage into GEO	12	confirmed	Mr. Marco Vietze	Universität der Bundeswehr München	Germany
8	Enhancement of Thermal Control Performance by Using Liquid Metal Radiator	12	confirmed	Mr. Tae-Yong Park	Chosun University	Korea, Republic of
9	A trade-off study on the mechanical support structure of the MASCOT-2 small body lander package	12	confirmed	Mr. Michael Lange	DLR (German Aerospace Center)	Germany
10	Qualification of an Infrared Array Based on NiCr Strips for CBERS 4A Satellite’s Space Simulation Test	12	withdrawn	Mr. George Fernandes	National Institute for Space Research - INPE	Brazil
11	design and on-board validation of pumped two-phase fluid loop for high heat flux removal	12	confirmed	Dr. xingang yu		China
12	The design of a satellite with a structure of Rubik's cube	12	withdrawn	Ms. Qi Chen	CAST	China
13	compression failure mechanisms in sandwich panels with corrugated channel cores	12	confirmed	Mr. Zhenyu Zhao	Xi'an Jiaotong University	China
14	Aeroheating Analysis of RCS Jet Interaction Effects on the RLV	12	confirmed	Dr. Xiaoyan Li	CALT,CASC	China
15	European REACH legislation: Impact on European launchers and current activities on new sustainable technologies		confirmed	Ms. Marie-Christine Contino	European Space Agency (ESA)	France

session 7

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