session 5

Title

Future Space Transportation Systems Technologies

Description

Discussion of technologies enabling new reusable or expendable launch vehicles and in-space transportation systems. Emphasis is on hardware development and verification before flight.

Date

2013-09-25

Time

14:45

Room

311B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

ESA FLPP SYSTEM DRIVEN TECHNOLOGY SELECTION FOR FUTURE EUROPEAN LAUNCH VEHICULES

accepted

18'

withdrawn

Mr. Guy Ramusat

ESA european space agency

France

2

long duration cryogenic propellant in-space storage technology

accepted

18'

confirmed

Mr. Wang Xiaowei

China Academy of Launch Vehicle Technology (CALT)

China

3

DESIGN OF INTER TANK STRUCTURE FOR CRYO STAGE WITH A COMMON BULK HEAD

accepted

18'

confirmed

Dr. REMESH KUMAR RADHA KRISHA REDDIAR

Vikram Sarabhai Space Centre, Thiruvananthapuram-695 022, INDIA

India

4

Optimization analysis of self-pressurization process for liquid oxygen tank of liquid rocket

accepted

18'

confirmed

Mr. Zhenqi Niu

Beijing Institute of Aerospace Systems Engineering

China

5

system design and technical demonstrations for reusable sounding rocket

accepted

18'

confirmed

Dr. Satoshi Nonaka

Japan Aerospace Exploration Agency (JAXA)

Japan

6

study on real-time network for reusable sounding rocket

accepted

18'

withdrawn

Mr. Takanori Narita

Mitsubishi Heavy Industries, Ltd.

Japan

7

prognostics and health management technology of large launch vehicle

accepted

18'

confirmed

Mr. shaohua zhang

China Academy of Launch Vehicle Technology(CALT)

China

8

CONCEPT OF MULTIPURPOSE ELECTROJET SPACE TUG CREATION

accepted

18'

confirmed

Mrs. Angela Oliinykova

Yuzhnoye State Design Office

Ukraine

9

Analysis of the avionic system achitecture for future manned reusable launch vehicle

accepted

18'

confirmed

Mrs. Wang Linna

China Academy of Launch Vehicle Technology (CALT)

China

10

Precise margins to operational limits of the RACS taking into account the PWM implementation

accepted

18'

Mr. Keysmer Enrique Damo La Rosa

University of Rome “La Sapienza”

Italy