session 3

Title: Upper Stages, Space Transfer, Entry and Landing Systems
type: oral
Description: Discussion of existing, planned or new advanced concepts for cargo and human orbital transfer. Includes current and near term transfer, entry and landing systems, sub-systems and technologies for accommodating crew and cargo transfer in space.
Date: 2013-09-24
Time: 14:45
Room: 311B

IPC members

Chairman: Mr. Shayne Swint, National Aeronautics and Space Administration (NASA), Marshall Space Flight Center, United States;
Chairman: Dr. Oliver Kunz, Beyond Gravity, Switzerland;
Rapporteur: Dr. Gennaro Russo, Associazione Italiana di Aeronautica e Astronautica (AIDAA), Italy;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		Aerothermodynamic and TPS Design Analysis of the USV3 Re-Entry Vehicle	accepted	15'	confirmed	Dr. Davide Cinquegrana	CIRA Italian Aerospace Research Centre	Italy
2		ATV Propulsion System - Welcome on board! How the ATV missions' feedback and real-time monitoring have been managed in a continuous improvement process	accepted	15'		Mr. Johann HENOCQUE	Airbus DS GmbH	Germany
3		Mission Concept and Technical Subjects of HTV-R (HTV-Return)	accepted	15'	withdrawn	Mr. Yusuke Suzuki	Japan Aerospace Exploration Agency (JAXA)	Japan
4		CARAVAN Cargo Autonomous Rendezvous And Velocity Adjustment/Navigation	accepted	15'	confirmed	Mr. Udrivolf Pica	International Space University (ISU)	Russian Federation
5		A Study of Reentry Blackout Alleviation Using Electron Bunching in the Reentry Plasma Layer	accepted	15'	withdrawn	Mr. Siddharth Krishnamoorthy	Student	United States
6		Applied Magneto-aerodynamics for safer re-entry of space vehicle.	accepted	15'	confirmed	Mr. Aakash Chhunchha	SRM University, Chennai	India
7		Aerothermodynamics of an Optimal Design of Mars Re-Entry Vehicle from Hypersonic to Subsonic Flow Regime	accepted	15'	withdrawn	Mr. Balbir Singh	Manipal Institute of Technology, Manipal University	India
8		Modeling and Analyzing of the Soft-landing Phase of Parachute-Retrorocket System	accepted	15'	confirmed	Mr. Huang Wei	Beijing Institute of Mechanical & Electrical Engineering	China
9		Scheme design of a parachute recovery system for UAV	accepted	15'	confirmed	Dr. Jingqi Cai	China Academy of Launch Vehicle Technology (CALT)	China
10		Design philosophy for OTV operating on cryogenic propellant components	accepted	15'		Mr. Dmitry Loupiak	Energia RSC	Russian Federation
11		Space Launch System Evolvability Assessment: Upper Stage Definition	accepted	15'		Mr. Jon Holladay	NASA	United States