session IP

Title: Interactive Presentations
type: interactive
Description: Authors with an abstract accepted for an interactive presentation will be asked to prepare slides and display them for the duration of the congress on plasma screens. Authors will be assigned to interactive sessions in which they must be near the plasma screens to engage in interactive discussions with other congress attendees.
Date: 2016-09-28
Time: 13:15
Room: Jalisco Hall C - Exhibition Hall

IPC members

Coordinator: Mr. Christophe Bonnal, European Conference for Aero-Space Sciences (EUCASS), France;
Coordinator: Mr. Daniel L. Dumbacher, American Institute of Aeronautics and Astronautics (AIAA), United States;

papers
Paper title	Presentation status	Speaker	Affiliation	Country
A STANDARD SPACE TRANSPORTATION AND INFRASTRUCTURAL SYSTEM FOR AN AFFORDABLE THREE STEPS PATH TO MARS MANNED MISSIONS		Mr. Giorgio Gaviraghi	Unispace Exponential Creativity	Italy
Lunar based mass driver applications	confirmed	Mr. Manfred Ehresmann	Institute of Space Systems, University of Stuttgart	Germany
Real-time Data Acquisition Platform using the OpenRocket Simulator	confirmed	Mr. Roberto Aguilar	Central American Association for Aeronautics and Space (ACAE)	Costa Rica
RING ROCKETS	confirmed	Mr. Oleg Aleksandrov	AVIASTAR Inc www.aviastar.us	United States
Numerical Investigations on Aerodynamic Drag Reduction of High Altitude and High Speed Vehicles using an Energy Deposition Method	confirmed	Dr. Daixian Zhang	China Aerodynamics Research and Developement Center	China
METHODOLOGICAL APPROACH FOR SUPPORT OF ROCKET COMPLEXES RESISTANCE TO EXTERNAL FACTORS	confirmed	Mr. Olexandr Kashanov	Yuzhnoye State Design Office	Ukraine
Case Study: Design of a Spaceport in Southern Hemisphere for Space Tourism Viability		Dr. Ugur Guven		United States
requirement analysis of space transporting system served for application mission of the space station	withdrawn	Dr. Kouan Hao	Aerospace System Engineering Shanghai, China	China
the infinite staging rocket – pulse mode testing	withdrawn	Prof.Dr. Vitaly Yemets	Oles Honchar Dnipropetrovsk National University	Ukraine
Particle Swarm Optimization Based PI Controller Design for Servo Actuation System of Reusable Launch Vehicle		Mrs. PRIYA KURIAN	ISRO	India
A Model-Based approach to the preliminary design of a space tug aimed at early requirement's verification	confirmed	Ms. Sara Cresto Aleina	Politecnico di Torino	Italy
trajectory,propulsion&general parameters optimization for suborbital launch vehicle	withdrawn	Mr. Shijie Sun	CALT,CASC	China
Multidisciplinary Shape Optimization of Future Re-usable Space Vehicle	withdrawn	Mr. Sagar Satpathy	Politecnico di Milano	Italy
Metamodel-Based Simulation Optimization of a Two Stage Liquid Propulsion Based Space Transportation System	withdrawn	Prof. Mehran Mirshams	K. N. Toosi University of Technology	Iran
advantages and prospect of multi-satellite launching upper-stage	confirmed	Mr. Xubin Zhang	Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)	China

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