session 3

Title

Upper Stages, Space Transfer, Entry and Landing Systems

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

2014-09-30

Time

14:45

Room

701B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Extending NASA Planetary Science Capability with an Improved Affordable Upper Stage

accepted

18'

withdrawn

Mr. Kevin Kelleher

Aerojet Rocketdyne

United States

2

Preferred design of a new cryogenic upper stage for Vega Evolution

accepted

18'

confirmed

Mr. Aicke Patzelt

MT Aerospace AG

Germany

3

System Costs Reduction Driven by Innovative Solutions - The Case of a Small Upper Stage Liquid Rocket Development

accepted

18'

confirmed

Dr. Celio Costa Vaz

Orbital Engenharia Ltda

Brazil

4

role of high thrust liquid propulsion stages in human exploration of the solar system

accepted

18'

confirmed

Mr. Mathias Rohrbeck

OHB System AG-Bremen

Germany

5

Progress in Developing a LOX/Methane Nanosatellite Launch Vehicle

accepted

20'

confirmed

Mr. Scott Claflin

Aerojet Rocketdyne

United States

6

Status of the MPCV European Service Module Propulsion Subsystem after Preliminary Design Review

accepted

18'

confirmed

Mr. Markus Jäger

Astrium Space Transportation

Germany

7

Electric Orbit Raising - Advantages, Transfer Aspects, Solutions

accepted

18'

confirmed

Mr. Francesco Cremaschi

Astos Solutions GmbH

Germany

8

Solar Electric Cargo Transportation for Human Exploration Beyond Low Earth Orbit

accepted

18'

confirmed

Mr. Joe Cassady

Aerojet Rocketdyne

United States

9

application of telescopic gear to lunar/planetary exploration spacecraft with base-extension separation mechanism

accepted

18'

confirmed

Mr. Naoaki Saeki

Nagoya University

Japan

10

aerodynamic analysis of an unmanned aerial vehicle at hypersonic speed

accepted

18'

no-show

Dr. Giuseppe Pezzella

CIRA Italian Aerospace Research Centre

Italy