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: 2014-10-02
Time: 14:45
Room: 713A

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	CONCEPTUALIZATION OF DESIGN MODIFICATIONS IN RE-ENTRY VEHICLES - VECTORING FOR REDIRECTION OF PLASMA	12'	confirmed	Ms. Poonampreet Kaur Josan	University of North Dakota	United States
2	Heat Transfer Management by Aerospikes for a Hypothesized Lifting Body in Hypersonic Flow	12'	confirmed	Dr. Shashank Khurana	Peking University	China
3	lift-to-drag ratio requirement analysis including low altitude guidance for re-entry flight of vtol vehicle	12'	withdrawn	Mr. Takushi Sakamoto	The University of TOKYO, Graduate school	Japan
4	The 3 Omega Transient Line Method for Thermal Characterization of Superinsulator Materials Developed for Spacecraft Thermal Control	12'	confirmed	Dr. Matthew Dalton	Sonaca Space GmbH	Germany
5	Low orbit environment effects on Carbon/SiC composites: experimental and numerical approach	12'	confirmed	Dr. Marta Albano	Sapienza University of Rome	Italy
6	Thermo-Mechanical Concept for a Modular On-Orbit-Serviceable Satellite System	12'	confirmed	Mr. Thomas A. Schervan	RWTH Aachen University - Institut fuer Leichtbau	Germany
7	design, build and experimental study of emergency power assist system	12'	withdrawn	Mr. Marshal Deep Kafle	Sacheon Aerospace Manufacturing Ind. Co. Ltd. (SAMCO)	Korea, Republic of
8	Parametric tool for the thermal analysis of a satellite.	12'	confirmed	Ms. Giulia Paoli		Switzerland
9	active thermal control system for venusian lander. new proposal	12'	confirmed	Mr. Anton Burdanov	Central Research Institute for Machine Building (FGUP TSNIIMASH)	Russian Federation
10	Potential advantages of the Space Vehicles with nuclear power - plant on board when dealing with global problems of modern age	12'	confirmed	Dr. Mykola M. Slyunyaev	Yuzhnoye State Design Office	Ukraine
11	Conceptual Design of a new Hybrid Capsule for manned Atmospheric Re-entry applications	12'	confirmed	Dr. Darryl Michael Cappadocia	University of Rome "La Sapienza"	Italy
12	Investigation of Heatshield Shape Changes on Optimum Aerodynamic Design for a Mars Entry Capsule	12'	confirmed	Mr. Bingyan Chen	China Academy of Aerospace Aerodynamics (CAAA)	China
13	characterization of high intensity sun radiation for tv-tb testing in a large vacuum facility	12'	confirmed	Mr. Matteo Appolloni	ESA	The Netherlands

session 7

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