IAF Digital Library

4

session 4

Title: Future Space Transportation Systems
Description: Discussion of future overall system designs and operational concepts for both expendable and reusable systems for Earth-to orbit transportation and exploration missions
Date: 2017-09-27
Time: 14:45
Room: Hall O

IPC members

Co-Chair: Mr. José Gavira Izquierdo, European Space Agency (ESA), The Netherlands;
Co-Chair: Mr. Charles E. Cockrell Jr., National Aeronautics and Space Administration (NASA), United States;
Rapporteur: Mrs. Philippa Davies, Reaction Engines Ltd., United Kingdom;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		HTV-X system integration plan	18	confirmed	Mr. daisuke tsujita	Mitsubishi Heavy Industries Ltd. - Nagoya Aerospace Systems	Japan
2		Ariane Next : weighting options for the next generation of Ariane launchers.	18	confirmed	Mr. Jerome VILA	Centre National d'Etudes Spatiales (CNES)	France
3		Evaluation of Future Ariane Reusable VTOL Booster Stages	18	confirmed	Mr. Etienne Dumont	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
4		Systematic Assessment of Reusable First-Stage Return Options	18	confirmed	Dr. Martin Sippel	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
5		DREAM CHASER FOR EUROPEAN UTILIZATION (DC4EU): ESA PILOT PHASE RESULTS	18	confirmed	Dr. Marco Berg	OHB System	Germany
6		Development plan and demonstration of Japanese reusable launch vehicle	18	confirmed	Mr. Kotaro Aoki	Mitsubishi Heavy Industries Ltd. Japan	Japan
7		design and ground test of an rbcc based two-stage-to-orbit reusable launch vehicle	18	confirmed	Dr. Chunlin Gong	Northwestern Polytechnical University，NPU	China
8		A Conceptual Analysis and Comparison of a Two-Stage-To-Orbit Reusable Launch Vehicle Using Airbreathing Precooling Hypersonic Engines	18	no-show	Dr. Jianxing Zhou	Beijing Aerospace Technology Institute	China
9		A feasibility study and conceptual proposal of a reusable multistage winged space transportation system with tandem orbiter-carrier connection by horizontal take-off and landing	18	confirmed	Mr. Yang Tianyang	Moscow Aviation Institute (National Research University, MAI)	Russian Federation
10		Multidisciplinary Shape Optimization of Reusable Space Vehicle	18	withdrawn	Mr. Sagar Satpathy	Politecnico di Milano	Italy
11		Preliminary Design for Modular SEP Tug Utilizing Dream Chaser Cargo Module	18	confirmed	Mr. Jonathan Grimm	The Ohio State University College of Engineering	United States