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: 2013-09-26
Time: 14:45
Room: 306B

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	Parametric Shape Optimization of Reentry Module for Space Missions	15'		Dr. Ugur Guven		United States
2	Thermal modeling of the adaptive thermal control microsystem of the spacecraft	15'	confirmed	Mr. Anatoliy Patsievskiy	S.P. Korolev Rocket and Space Corporation Energia	Russian Federation
3	Global error estimation in CFD mesh coarsening process for uncertainty quantification methods	15'	confirmed	Mr. Martin Kubicek	University of Strathclyde	United Kingdom
4	Cooling system for high energy potential space vehicle	15'	confirmed	Mr. Anton Burdanov	Central Research Institute for Machine Building (JSC TSNIIMASH)	Russian Federation
5	Heat Transfer Management by Aerospikes for a Hypothesized Lifting Body in Hypersonic Flow	15'	withdrawn	Dr. Shashank Khurana	The University of TOKYO, Graduate school	China
6	aerodynamic improvement of the brazilian satellite launch vehicle	10'	confirmed	Mr. Col. Jose Duarte	Instituto de Aeronáutica e Espaço (IAE)	Brazil
7	Numerical study of active cooling techniques of a nano satellite using CFD for performance enhancement	10'	confirmed	Mr. Mollik Nayyar	Manipal Institute of Technology, Manipal University	India
8	Aerodynamic Design of a Capsule Configuration for High-speed Manned Re-entry	10'	confirmed	Mr. Bingyan Chen	China Academy of Aerospace Aerodynamics (CAAA)	China
9	variable inertia fluidic ring actuator on attitude control and residual fuel management systems	10'	confirmed	Ms. Hong Guan	Beihang University	China
10	the study on iot based manufacturing system for astronautical products	10'	confirmed	Mr. Xie Xinping	Nanjing University of Aeronautics and Astronautics	China
11	Thermal Mapping and Trends of Mars Analog Materials in Sample Acquisition Operations Using Experimentation and Models	10'	confirmed	Mr. Timothy Szwarc	Stanford University	United States
12	Transient study about the heat transfer of sublimator combined with fluid loop	10'	confirmed	Dr. Yuying WANG	Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology	China
13	Materials surface emissivity analyses performed by the combined use of dual and single color optical pyrometers	10'	confirmed	Dr. Carlo Purpura	CIRA Italian Aerospace Research Centre	Italy

session 7

Order

Time

Paper title

Mode

Presentation status

Speaker

Affiliation

Country