session 7

Title: Space Vehicles – Mechanical/Thermal/Fluidic Systems
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 (JSC 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
4	Chemical non equilibrium simulations of hypersonic flights in carbon dioxide-nitrogen atmospheres using a coupled Euler-second-order boundary layer method	15'	withdrawn	Mr. Martin Starkloff	University of the Federal Armed Forces Munich	Germany
5	Re-Use of EXOMARS rover on icy moons of Jupiter	15'	withdrawn	Mr. Abrar-Ul-Haq Khan Baluch	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
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
8	Uncertainty quantification for hypersonic flow simulations	15'	withdrawn	Mr. Jeroen Cappaert	International Space University (ISU)	France
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
10	Solid rocket booster segment joint - a parametric study	15'	withdrawn	Mr. SHITIJ ARORA	Vikram Sarabhai Space Centre (VSSC)	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
12	Robust neural network control of space robot system with flexible joints	15'	no-show	Dr. Zhiyong Chen		China
13	Effect of forebody configuration on nonslender delta wing rock	Poster	withdrawn	Mr. Bing Han	College of Astronautics, Northwestern Polytechnical University	China
14	Computational analysis of thermal and structural loads on re-entry vehicles and a conceptual SSTO model using an in-house solver code.	Poster	withdrawn	Mr. Shrrirup Nambiar	DEFENCE INSTITUTE OF ADVANCED TECHNOLOGY	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
24	Modeling of hydrogen embrittlement at steady state at high temperature using a commercial finite element program	Poster	withdrawn	Dr. Wissam Bouajila	DLR, German Aerospace Center	Germany
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
–	Aerothermal Analysis of Ultra High Temperature Ceramics Flying Test Bed	with 14761		Dr. Mario De Stefano Fumo	CIRA Italian Aerospace Research Centre	Italy

session 7

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