session 4

1

NELS - Launcher concept selection for the “New European Launch Service”

15'

confirmed

Mr. Marc Scheper

OHB System AG-Bremen

Germany

2

Economical self-sustainability of a New European Launch Service (NELS)

15'

Mr. Piotr Perczynski

MT Aerospace AG

Germany

3

Conceptual design of a Space Tug for satellites missions support

15'

confirmed

Dr. Maria Antonietta Viscio

Politecnico di Torino - Thales Alenia Space Italia

Italy

4

Design parameters optimisation of the unified series of reusable interorbital tug with electrical propulsions and nuclear power system of megawatt class in near earth transport operations for heavy payloads and sattelite transportation to f

15'

Mr. Dmitry Goropaev

Central Research Institute for Machine Building (FGUP TSNIIMASH)

Russian Federation

5

Progress of SpaceLiner Rocket-Powered High-Speed Concept

15'

confirmed

Dr. Martin Sippel

Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

Germany

6

Progress on the SKYLON and SABRE

15'

confirmed

Mr. Mark Hempsell

Reaction Engines Ltd.

United Kingdom

7

Analysis of Effectiveness of Utilization Strategy for Space Launch Vehicle with Reusable First Stage in Turnaround Servicing Phase

15'

confirmed

Mrs. Alla Serikova

Central Research Institute of Machine Building (FSUE/TSNIIMASH)

Russian Federation

8

The Conceptual Scheme Based on Air-breathing Propulsion Reusable Space Transportation System

15'

confirmed

Ms. Yingshan Xu

Beijing Electro-Mechanical Engineering Institute

China

9

System-defined flight demonstrator of reentry launch vehicle’ block within reusable space launch vehicle configuration

15'

Dr. Anatoly Kuzin

Khrunichev State Research & Production Space Center

Russian Federation

10

The Austral Launch Vehicle: Reducing Space Transportation Cost Through Reusability, Modularity and Simplicity

15'

confirmed

Mr. Adriaan Schutte

Heliaq Advanced Engineering

Australia

11

Optimum Maneuver of Air Launch Rockets

15'

confirmed

Mr. Masashi Miura

Tottori University

Japan