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: 2018-10-04
Time: 14:45
Room: ÖVB 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	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	14:45	Automated Thermal Model Correlation Tool for Space Applications	12	confirmed	Mr. Alexander Milke	ArianeGroup	Germany
2	14:57	Optimum Design and Thermal Analysis of Composite Insulation Structure Used in Cryogenic Storage Tanks on-orbit	12	withdrawn	Mr. shaohua zhang	China Academy of Launch Vehicle Technology(CALT)	China
3	15:09	Micro-pumped cooling loop to standardize micro-sat thermal control	12	confirmed	Mr. Johannes van Es	Netherlands Aerospace Centre (NLR)	The Netherlands
4	15:21	A backup system of a satellite orientation based on inverse problems technique	12	confirmed	Prof. Aleksey V. Nenarokomov	Moscow Aviation Institute	Russian Federation
5	15:33	Evaluation of thermal analysis of orbital environment of microsatellite ALE-1	12	confirmed	Ms. Mina Konaka	Tohoku University	Japan
6	15:45	The way of defining a powerful method for supersonic and hypersonic winged spacecraft aerodynamics prediction	12	confirmed	Mrs. Olena Koliada	Yuzhnoye State Design Office	Ukraine
7	15:57	Thermal Loads Simulators and Setup Strategies of Thermal Tests for Small Satellites	12	confirmed	Mr. Roy Stevenson Soler Chisabas	Brazilian National Institute for Space Research - INPE	Brazil
8	16:09	Unsteady Coupled Heat Transfer Simulations of Hypersonic Gap Flows	12	withdrawn	Dr. Qiang Wang		China
9	16:21	Using the “Comparative Test Method” to Determine the Heat Statuses for the Heat Shields of Spacecraft	12	confirmed	Mr. Yang Tianyang	Moscow Aviation Institute (National Research University, MAI)	Russian Federation
10	16:33	Experimental and Numerical Study on the PCM Thermal Control Device for Spacecraft Electronics	12	confirmed	Prof. Taig Young Kim	Korea Polytechnic University	Korea, Republic of
11	16:45	Thermal Control of High Power Applications on CubeSats	12	confirmed	Ms. Katja Janzer	Technische Universität München	Germany
12	16:57	The Influence of Shock Wave on Ablation Thermal Environment of Re-entry Vehicle Protuberance	12	confirmed	Mr. dongbin ou	China Academy of Aerospace Aerodynamics (CAAA)	China

session 7

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