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: 2016-09-29
Time: 14:45
Room: Salon de Eventos 1

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	Future Actuator development - a new approach and first results	15'	confirmed	Dr. Oliver Kunz	RUAG Space AG	Switzerland
2	Nanostructured rigid foams for space applications	15'	withdrawn	Dr. Tomas Vlcek	TOSEDA s.r.o.	Czech Republic
3	the thermal analysis of lapan’s ir micro bolometer optical design	15'	confirmed	Mr. Bustanul Arifin	Indonesian National Institute of Aeronautics and Space (LAPAN)	Indonesia
4	Study on a novel self-adaptive spacecraft thermal control system with motorized thermal shade and loop heat pipe	15'	no-show	Dr. Dong La	Shanghai Institute of Satellite Engineering	China
5	Numerical Analysis of Integrated Model of Flow Field and Carbon/Carbon Structure for Temperayure Response in Arc Tunnel	15'	withdrawn	Dr. Zhaowei Wang	China Academy of Launch Vehicle	China
6	Thermal Modeling and Simulation for ‘Pratham’ IIT Bombay Student Satellite	15'	no-show	Mr. Ratnesh Mishra	Indian Institute of Technology	India
7	Quick Design Tool for Stratification Processes in Cryogenic Fuel Tanks with Focus on Sandwich Common Bulkheads	15'	confirmed	Mr. Marco Vietze	Universität der Bundeswehr München	Germany
8	Parameter study of Lap structure between Skirt and Composite Material Case of SRM	15'	withdrawn	Mr. wang liqiang	The 41st Institute of Academy of China Aerospace Science and Technology Corporation	China
9	Thermal-Vacuum Tests of the Amazonia-1 Satellite TM Performed at INPE With Success	15'	confirmed	Dr. Jose Sergio Almeida	The Brazilian Institute for Space Research - INPE	Brazil
10	Waverider design and analysis based on shock-fitting method	15'	confirmed	Prof. Bingyan Chen	China Academy of Aerospace Aerodynamics (CAAA)	China

session 7

Order

Time

Paper title

Mode

Presentation status

Speaker

Affiliation

Country