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: 2012-10-04
Time: 15:15
Room: TS07 (Sala Regulus, Hall 3)

IPC members

Chairman: Dr. Brij Agrawal, Naval Postgraduate School, United States;
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	Recent Thermal Design Driven Development Activities at MT Aerospace	15'	confirmed	Dr. Farid Infed	MT Aerospace AG	Germany
2	Cryogenics tasks in perspective Russian scientific space projects	15'	confirmed	Mr. Anton Burdanov	Central Research Institute for Machine Building (FGUP TSNIIMASH)	Russian Federation
3	Coating effects on thermal properties of carbon carbon and carbon silicon carbide composites for space thermal protection systems.	15'	confirmed	Dr. Marta Albano	Sapienza University of Rome	Italy
6	EXPERT – The ESA Experimental Re-Entry Vehicle: Experiments and Payloads qualified and ready for the flight	15'	confirmed	Dr. Antonio Del Vecchio	CIRA Italian Aerospace Research Centre	Italy
7	Large Scientific Satellite Tested with Success at LIT-INPE 6m x 8m Space Simulation Chamber	15'	confirmed	Dr. Jose Sergio Almeida	Instituto Nacional de Pesquisas Espaciais (INPE)	Brazil
9	Effect of Eccentricity on the Heat Transfer Rates of a Re Entry Vehicle with Concave Windward Surface	15'	confirmed	Mr. Gurunadh Velidi	University of Petroleum and Energy Studies	India
11	Aerothermodynamics of a Hemispherical-Cylindrical Blunt Vehicle with a Flow through Duct	15'	confirmed	Mr. Gurunadh Velidi	University of Petroleum and Energy Studies	India
15	Numerical analysis of engine cylinder liner with inner functionally graded thermal barrier coating	Poster		Mrs. Lihong Yang	Harbin Engineering University	China
16	The Hungarian CoCoRAD experiment in the BEXUS program of the ESA	Poster	confirmed	Mr. Balazs Zabori	Budapest University of Technology and Economics	Hungary
17	Aeroheating and Structure Coupled Analysis in Thermal Protection System for Reusable Launch Vehicle	Poster	confirmed	Mr. Shiyong Huang	China Academy of Launch Vehicle Technology (CALT)	China
18	Analysis of load transmission line on the fuselage of reusable launch vehicle	Poster	confirmed	Mrs. Ma Tingting	China Academy of Launch Vehicle Technology (CALT)	China
19	Simulation of multi-body separation of aerospace vehicles based on unstructured overset grids technology	Poster	confirmed	Mr. Zhou Liu	China Academy of Aerospace Aerodynamics (CAAA)	China
20	Correction of Hypersonic Viscous Interaction Correlation Parameter	Poster	confirmed	Mr. Gong Anlong		China
21	An all-speed unstructuredflow solver for separation process	Poster	confirmed	Mr. YueLong He	China Academy of Aerospace Aerodynamics (CAAA)	China
22	Numerical simulation of uav carrier-landing interactive flowfield	Poster	confirmed	Mr. YueLong He	China Academy of Aerospace Aerodynamics (CAAA)	China
23	Numerical simulation of aerodynamic heating on hypersonic slip flow	Poster	confirmed	Mr. Guo-hao DING	National University of Defense Technology	China
25	Acoustic-elastic of flight vehicle	Poster		Mr. pei xi	Northwestern Polytechnical University	China
26	Investigate of rudder deflected multi-body separation	Poster	confirmed	Dr. Dun Li	China Academy of Aerospace Aerodynamics (CAAA)	China

session 7

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