IAF Digital Library

5

session 5

Title: Technologies for Future Space Transportation Systems
Description: Discussion of technologies enabling new reusable or expendable launch vehicles and in-space transportation systems. Emphasis is on TRL hardware development and verification prior to flight, including ground testing and/or innovative technology prototype demonstrations not yet involving flight.
Date: 2017-09-28
Time: 09:45
Room: Hall O

IPC members

Co-Chair: Mr. Patrick M. McKenzie, MITSUI SEIKI KOGYO CO., LTD., United States;
Co-Chair: Dr. Giuseppe Rufolo, CIRA Italian Aerospace Research Centre, Italy;
Rapporteur: Prof. Lin Shen, China Academy of Launch Vehicle Technology (CALT), China;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		The Next Frontier: Transportation for the Cislunar Marketplace	15	confirmed	Dr. Melissa Sampson	United Launch Alliance LLC (ULA)	United States
2		Conceptual Design for Pulsed Arc Propelled Space Tug Services	15	confirmed	Dr. Patrick Neumann	Space Industry Association of Australia	Australia
3		Aerothermal Characteristics of a Gliding Reentry Vehicle with Low Ballistic Coefficient and High Lift-to-drag	15	confirmed	Prof.Dr. Yu Zhefeng	China Aerodynamics Research and Development Center (CARDC)	China
4		Technology demonstrations and system design for reusable rocket flight experiments	15	confirmed	Dr. Satoshi Nonaka	Japan Aerospace Exploration Agency (JAXA)	Japan
5		Developments on Low Cost Manufacturing Methods for Cylindrical Launcher Structures	15	withdrawn	Dr. Carina Dorbath	MT Aerospace AG	Germany
6		Ascent adaptive guidance for power system fault of heavy lift launch vehicle	15	withdrawn	Dr. Yepeng Han	School of Astronautics, Harbin Institute of Technology	China
7		Flight Path Design of a Reusable Rocket Flight Demonstrator	15	withdrawn	Mr. Shunsuke Sato	Japan Aerospace Exploration Agency (JAXA)	Japan
8		Parachute-landing recovery technology of Launch vehicle stage	15	confirmed	Mr. Shengbao Wu		China
9		Update on Risk Reduction Activities for a Liquid Advanced Booster for NASA’s Space Launch System	15	confirmed	Mr. Andrew Crocker	Dynetics	United States
10		a hydrogen-turbo-pump-powered thrust vector control servo system for high thrust liquid-hydrogen-liquid-oxygen rocket engines	15	confirmed	Mr. Guanghui Jing	China Academy of Launch Vehicle Technology (CALT)	China
11		ARIANE 6 - New Aerostructures for the new European Launcher	15	confirmed	Mr. Aicke Patzelt	MT Aerospace AG	Germany
12		Numerical Research on the Separation Process of Launch Vehicle's Boosters with the Impingement of Multiple Nozzle Plumes of its Core Stage	15	withdrawn	Dr. Zhenhai Wanyan	Beijing institute of Astronautical System Engineering, Beijing	China
13		Research and Development of Revolutionary Low Cost Space Transportations for Space Infrastructure Constructions	15	confirmed	Prof. Yoshiki Yamagiwa	Shizuoka University	Japan