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: 2011-10-06
Time: 15:00
Room: TS-17

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	A new methodology for estimating surface heat flux from in-depth sensors	15	confirmed	Dr. Jay Frankel	University of Tennessee	United States
2	Carbon/carbon comparative optimization method for hot structures applications in re-entry environment conditions	15	confirmed	Dr. Marta Albano	Sapienza University of Rome	Italy
3	Active thermal control system for perspective venusian lander	15	confirmed	Mr. Anton Burdanov	Central Research Institute for Machine Building (FGUP TSNIIMASH)	Russian Federation
4	A Thermal Model for Analysis and Control of Drilling in Icy Formations on Mars	15	confirmed	Mr. Timothy Szwarc	Stanford University	United States
5	Egse in spacecraft thermal vacuum tests for accurate power measurements and minimization of power supplies	15	confirmed	Dr. Durval Zandonadi Jr.	Instituto Nacional de Pesquisas Espaciais (INPE)	Brazil
6	Application of inertia relief in structural strength analysis of reusable launch vehicle	15	withdrawn	Mrs. Ma Tingting	China Academy of Launch Vehicle Technology (CALT)	China
7	RE-USE OF EXOMARS ROVER ON ICY MOONS OF JUPITER	15	withdrawn	Mr.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
8	Versions of orbiters’ flight systems for nonnuclear action on asteroid Apophis	15	confirmed	Dr. Mykola M. Slyunyaev	Yuzhnoye State Design Office	Ukraine
9	Spacecraft Aerodynamics and Heat Shield Characteristics Impact on Optimal Aeroassisted Coplanar Orbital Transfer	15	confirmed	Dr. Antonio Mazzaracchio	Sapienza Università di Roma	Italy
10	Thermal buckling of simply supported moderately thick functionally graded plates	15	confirmed	Ms. Yang Lihong		China
11	Research on Flight experiment Technique to Verification Thermal Protection Materials and Insulation Materials	15	withdrawn	Dr. Yu Yubin	China Academy of Launch Vehicle Technology (CALT)	China
12	Application of Structured Singular Value Method to Aeroservoelastic Robustic Stability Analysis for Reusable Launch Vehicle	15	no-show	Mr. Junpeng Hui	China Academy of Launch Vehicle Technology (CALT)	China
13	Flow-Structure-Thermal Investigation of Blunt Body in High-Enthalpy Flows	15	no-show	Mr. Jing Yang	College of Aerospace and Materials Engineering, National University of Defense Technology	China

session 7

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