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: 2010-09-30
Time: 15:15
Room: Meeting Room 42

IPC members

Chairman: Prof. Mario Marchetti, Sapienza University of Rome, Italy;
Chairman: 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	CDR-Level Structural Modelling And Optimization Of The Mercury Sodium Atmosphere Spectral Imager (MSASI)	10	confirmed	Mr. Joao Ricardo	Sonaca Space GmbH	Portugal
2	computational fluid dynamics analysis and flow test of manned spacecraft	15	confirmed	Mr. Wei Lu	China Academy of Space Technology (CAST)	China
3	COMPUTATIONAL MODELLING OF HEAT TRANSFER IN A SPACECRAFT HEAT PIPE.	10	confirmed	Mr. Michael Kio	National Space Research and Development Agency (NASRDA)	United Kingdom
4	Coupled aeroassisted orbital plane change manoeuvre and thermal protection system optimization	15	confirmed	Dr. Antonio Mazzaracchio	Sapienza Università di Roma	Italy
5	Destructive materials thermal properties determination with application for spacecraft structures testing	15	confirmed	Prof. Oleg Alifanov	Moscow Aviation Institute	Russian Federation
6	enabling technologies for hot structures of next generation rlv's - the asa program summary	15	confirmed	Mr. F.A. Fossati	Aviospace S.R.L	Italy
7	Experimental and Numerical Studies of Spallation Particles Ejected from a Light-weight Ablator	10	confirmed	Mr. Sohey Nozawa	Kyushu University	Japan
8	effective parameters on calculation of effective thermal conductivity of multilayer printed circuit boards in space application	10	confirmed	Mr. Esmaeil Moeini	Amirkabir University of Technology, AutSat Project	Iran
9	IBDM: The International Berthing Docking Mechanism For Human Missions to Low Earth Orbit and Exploration	15	confirmed	Mr. Marco Caporicci	European Space Agency (ESA)	The Netherlands
10	Optical sensor system applicability for spacecraft tests	10	confirmed	Mr. Alfonso Giusti	University of Rome “La Sapienza”	Italy
11	Research on the thermal control hardware combined with heat pipe and phase change material	15	confirmed	Prof. Taig Young Kim	Korea Polytechnic University	Korea, Republic of
12	Surface Heat Flux Estimation and New Calibration Methods For Ground-Based Testing in Hypersonic Environments	15	withdrawn	Dr. Jay Frankel	University of Tennessee	United States
13	Wing Leading Edge Ablation Tests in Arc Tunnel	15	confirmed	Dr. Bangcheng Ai	China Aerospace Science and Industry Corporation	China
14	results from the thermal balance testing of the cbers 3-4 satellite tm	10	confirmed	Dr. Marcio Bueno dos Santos	Instituto Nacional de Pesquisas Espaciais (INPE)	Brazil

session 7

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