PRELIMINARY PROGRAMME - Aventri...Detailed programme: Wednesday 12 June 2013 8h30-9h30 Opening Welcome addresses Michel Eymard, CNES, Paris, France 9h30-10h30 Plenary session 1 Chairs:

1

PRELIMINARY PROGRAMME This programme is liable to changes

Programme at a glance

08h30 08h30 09h00

Launch range facilities

Launch complex

Test facilities

Launch range facilities

Launch complex

Test facilitiesLaunch range

facilitiesLaunch

complexTest facilities

Session 3 - Specific technical aspects

Session 3 - Communications

- tracking stations

Session 3 - Sub systems

and techniques

Session 3 - Specific technical aspects

Session 3 - Communications

- tracking stations

Session 1 - Design and concepts

Coffee break

16h00 17h30

16h00 17h30

Session 1 - Space port

architecture - operations

Session 1 - Space port

architecture - operations

Session 2 - Maintenance

and exploitation

Session 2 - Exploitation - Operations

Session 2 - Exploitation - Operations

Session 2 - Environment - regulations -

safety

Session 2 - Environment - regulations -

safety

Lunch

14h00 15h30

14h00 15h30

Plenary session 1

Dining cocktail19h00 23h00

Session 3 - Sub systems

and techniques

Closing

09h00 10h30 09h30

11h30

Session 2 - Maintenance

and exploitation

Coffee break

Plenary session 2

Thursday 13 June 2013 Friday 14 June 2013

09h00 10h30

11h00 12h00

Plenary session 1

Welcome addresses

Welcome Welcome

11h00 12h30

Coffee break

Welcome

Session 1 - Design and concepts

Session 1 - Description and general

characteristics

Session 1 - Description and general

characteristics

Wednesday 12 June 2013

Opening

Lunch

Coffee break

Detailed programme:


8h30-9h30 Opening

Welcome addresses

Michel Eymard, CNES, Paris, France

9h30-10h30 Plenary session 1

Chairs: Michel Eymard and Bernard Brandt

O01 - Baikonur Proton Launch Operations

James Youdale

ILS, Belcastel, France

O02 – Soyuz in French Guiana: summary of a success story

Jean-Marc Astorg

CNES, Paris, France

10h30-11h00 The coffee breaks are sponsored by Telematic Solutions



O03 - Planning for the development

exploration launch vehicle

David Herst

NASA, Kennedy Space Center, United States

O04 - The Present and Trend of China’s Long March Vehicles Ground and Launch Systems Processing

Yinghong Qi

China Academy of LaunchVehicle Technology

12h00-14h00 The lunch is spo

Detailed programme:


Michel Eymard, CNES, Paris, France

Plenary session 1

Bernard Brandt

Baikonur Proton Launch Operations

Soyuz in French Guiana: summary of a success story

The coffee breaks are sponsored by Telematic Solutions

Plenary session 1

Bernard Brandt

Planning for the development of ground launch systems for the next generation NASA

United States

The Present and Trend of China’s Long March Vehicles Ground and Launch Systems Processing

Academy of LaunchVehicle Technology, Beijing, China

lunch is sponsored by APCO.

2

The coffee breaks are sponsored by Telematic Solutions Advanced.

of ground launch systems for the next generation NASA

The Present and Trend of China’s Long March Vehicles Ground and Launch Systems Processing

14h00-17h30 Launch Range Facilities

- operationsChairs: Michel Starozinski and Jacques Gigou

14h00 O05 - EGSE

Simon Klingler

CLEMESSY, Mulhouse

14h30 O06 - Principles of design and operations in the Vega Launch Range

Mauro Cardone

ESA, Frascati,

15h00 O07 - Spaceport design for safety

Jean-Pierre

CNES, Toulouse

15h30 The coffee breaks are sponsored by Telematic Solutions Advanced.

16h00 O08 - Conceptualization, Design and Layout of Propellant Facilities at a Man

Launch Pad

Prateep Basu

Indian Space Research Organization

16h30 O09 - A Digital Management Platform for Working Process Control in Rocket Launch

Field

Xie Zhifeng

China Academy of Launch Vehicle Technology (CALT)

17h00 O10 - Research on power supply and grounding system of Aerospace Launch Facility

Xiang Xiang

China Academy of Lauch Vehicle Technology

14h00-17h30 Launch Complex

Chairs: Pier-Michele Roviera and Jacques

14h00 O11 - Rocket Sled Track Facility as a Test Platform and a Launch Assist of Space Planes

Nakata Daisuke

Muroran Institute of Technology

14h30 O12 - Reuse of former launch complex

Marc Vales

CNES, Paris, France

15h00 O13 - Integrating Sustainable Practices into Ground Based Space Facilities

Mike McCarthy

Reynolds, Smith & Hills, Inc.

Launch Range Facilities - Session 1 - Space port architecture

operations Jacques Gigou

Klingler

Mulhouse, France

Principles of design and operations in the Vega Launch Range

Cardone

, Italy

Spaceport design for safety

Trinchero

Toulouse, France


Conceptualization, Design and Layout of Propellant Facilities at a Man

Basu

Indian Space Research Organization, Kolkata, India

A Digital Management Platform for Working Process Control in Rocket Launch

China Academy of Launch Vehicle Technology (CALT), Beijing, China

Research on power supply and grounding system of Aerospace Launch Facility

China Academy of Lauch Vehicle Technology, Bejing, China

Launch Complex - Session 1 - Design and concepts

Jacques Bertrand

Rocket Sled Track Facility as a Test Platform and a Launch Assist of Space Planes

Daisuke

Muroran Institute of Technology, Muroran-shi, Japan

Reuse of former launch complex

France

Integrating Sustainable Practices into Ground Based Space Facilities

McCarthy

Reynolds, Smith & Hills, Inc., Jacksonville, FL, United States

3

Space port architecture

Principles of design and operations in the Vega Launch Range


Conceptualization, Design and Layout of Propellant Facilities at a Man-rated

A Digital Management Platform for Working Process Control in Rocket Launch

China

Research on power supply and grounding system of Aerospace Launch Facility

Design and concepts

Rocket Sled Track Facility as a Test Platform and a Launch Assist of Space Planes

Integrating Sustainable Practices into Ground Based Space Facilities


16h00 O14 - A next generation launch complex for a next generation launcher: Ariane 6 AIT

facilities and Launch Pad

Christian Canart

CNES, Paris, France

16h30 O15 - An integrated Launch Vehicle

New European Launch System

Kate Underhill

MT Aerospace AG

17h00 O16 - An Analysis of the Design Requirements of General Assembly

Large Manned Spacecraft Launch Site

Zhao Ting

China Academy of Launch Vehicle Technology

14h00-17h30 Test Facilities

Chairs: Anja Frank and Jacques Tanguy

14h00 O17 - Cryogenic tests facilities and achievements for launcher tanks developments and

technologies

Sébastien Bianchi

Air Liquide Advanced

14h30 O18 - BEAP: A5 or VEGA Booster test Bench in flight position

Frédéric Munos

CNES, Kourou

15h00 O19 - Overall panorama of the test facilities in snecma vernon

Philippe Caisso

Safran Group


16h00 O20 - Multifunctional Robot Test Facility for On

Surface Exploration

Benjamin Girault

DFKI Robotics Innovation Center


next generation launch complex for a next generation launcher: Ariane 6 AIT

facilities and Launch Pad

Canart

France

An integrated Launch Vehicle – Launch Complex approach to development of a

New European Launch System

Underhill

MT Aerospace AG, Augsburg, Germany

An Analysis of the Design Requirements of General Assembly

Large Manned Spacecraft Launch Site

China Academy of Launch Vehicle Technology, Beijing, China

Test Facilities - Session 1 - Description and general characteristics

Jacques Tanguy

Cryogenic tests facilities and achievements for launcher tanks developments and

technologies

Bianchi

Air Liquide Advanced Technologies, Sassenage, France

BEAP: A5 or VEGA Booster test Bench in flight position

Munos

Kourou, France

Overall panorama of the test facilities in snecma vernon

Caisso

Safran Group - Snecma Space Engines Division, Vernon, France


Multifunctional Robot Test Facility for On-Orbit Operation and Extraterrestrial

Surface Exploration

Girault

DFKI Robotics Innovation Center, Bremen, Germany

4


next generation launch complex for a next generation launcher: Ariane 6 AIT

Launch Complex approach to development of a

An Analysis of the Design Requirements of General Assembly-test Building at

Description and general characteristics

Cryogenic tests facilities and achievements for launcher tanks developments and

BEAP: A5 or VEGA Booster test Bench in flight position

Overall panorama of the test facilities in snecma vernon


Orbit Operation and Extraterrestrial

16h30 O21 - PF52, Test facility for cryogenic subsystems and Vinci engine

Philippe Magnant

Snecma, Vernon

17h00 O22 - Altitude Engine Test Facility for Korea Space Launch Vehicle II 2nd Stage

Seung-Han Kim

Korea Aerospace Research Institute

Thursday 13 June 2013


- safety Chairs: Jean-Pierre Trinchero and Françoise Perrel

9h00 O23 - Reliable Propellant Service for Chemical Propulsion Spacecrafts, Hypergolic

Propellants, Ground Infrastructure, Propellant Handling

Stefan Ziegenhagen

Astrium GmbH Space Transportation

9h30 O24 - Chemical’s

Bruno Nicolas

VINCI Energies

10h00 O25 - Historical evolution of toxic propellant use and waste treatment for space

industry.

Jean-Francois

CNES, Toulouse


11h00 O26 - Regulating Spaceports for Commercial Sub

Jean-Bruno

European Aviation Safety Agency (EASA)

11h30 O27 - Skin mode

Clément Baron

CNES, Toulouse

12h00 O28 – Ground

Michael Wells

Government of Bermuda

PF52, Test facility for cryogenic subsystems and Vinci engine

Magnant

Vernon, France

Altitude Engine Test Facility for Korea Space Launch Vehicle II 2nd Stage

Kim

Korea Aerospace Research Institute, Daejeon, Korea

Thursday 13 June 2013

Launch Range Facilities - Session 2 - Environment

Françoise Perrel

Reliable Propellant Service for Chemical Propulsion Spacecrafts, Hypergolic

Propellants, Ground Infrastructure, Propellant Handling

Ziegenhagen

Astrium GmbH Space Transportation, Möckmühl, Germany

Chemical’s and pressurized equipment’s risks prevention

Nicolas

VINCI Energies, Saint Denis, France

Historical evolution of toxic propellant use and waste treatment for space

Francois Niccolai

Toulouse, France

breaks are sponsored by Telematic Solutions Advanced.

Regulating Spaceports for Commercial Sub-orbital and Orbital Flights

Marciacq

European Aviation Safety Agency (EASA), Cologne, Germany

Skin mode Doppler radar for safety mission

Baron

Toulouse, France

Ground-based space facilities in Bermuda

Wells

Government of Bermuda, Hamilton, Bermuda

5

PF52, Test facility for cryogenic subsystems and Vinci engine

Altitude Engine Test Facility for Korea Space Launch Vehicle II 2nd Stage Engine

Environment – regulations

Reliable Propellant Service for Chemical Propulsion Spacecrafts, Hypergolic

ed equipment’s risks prevention

Historical evolution of toxic propellant use and waste treatment for space

breaks are sponsored by Telematic Solutions Advanced.

orbital and Orbital Flights


Chairs: Christian Lardot and Pier-Michele Roviera

9h00 O29 - Evolution of ground control systems: Same functions, different known needs

Miguel Mañas

GTD, Barcelona

9h30 O30 - Industrie Cometto S.p.A.: the right ground support for the best result i

space.

Guido Beraudo

Industrie Cometto S.p.A

10h00 O31 - Use of Analytical Tools to Optimize Ground Operations and Processing

Jeremy Parsons

NASA, Kennedy Space Center


11h00 O32 - The Spaceport Multi

Spaceport Planning

Jeremy Parsons

NASA, Kennedy Space Center

11h30 O33 - Exploitation of the Soyuz launch pad in French Guiana

Francois Barreau

Arianespace,

12h00 O34 - Operation of the ARIANE 5 / ELA 3 launch complex

Christian Lardot

ARIANESPACE


Chairs: Frédéric Munos and Anja Frank

9h00 O35 - Statistical Methods for the evaluation of the quality of measurement data on the

test benches

Wolfgang Stuchlik

DLR, Hardthausen

9h30 O36 - -Maintenance of test facilities for rocket engines

Rainer Schürmanns

DLR e.V., Hardthausen

Launch Complex - Session 2 - Exploitation - Operations

Michele Roviera

Evolution of ground control systems: Same functions, different known needs

Mañas

Barcelona, Spain

Industrie Cometto S.p.A.: the right ground support for the best result i

Beraudo

Industrie Cometto S.p.A, Borgo San Dalmazzo, Italy

Use of Analytical Tools to Optimize Ground Operations and Processing

Parsons

Kennedy Space Center, United States


The Spaceport Multi-Flow Model: Utilizing Discrete Event Simulation for Future

Spaceport Planning

Parsons

Kennedy Space Center, United States

Exploitation of the Soyuz launch pad in French Guiana

Barreau

, Evry-Courcouronnes, France

Operation of the ARIANE 5 / ELA 3 launch complex

Lardot

ARIANESPACE, Evry Courcouronnes, France

Test Facilities - Session 2 - Maintenance & exploitation

Anja Frank

Statistical Methods for the evaluation of the quality of measurement data on the

test benches

Stuchlik

Hardthausen, Germany

Maintenance of test facilities for rocket engines

Schürmanns

Hardthausen, Germany

6

Operations

Evolution of ground control systems: Same functions, different known needs

Industrie Cometto S.p.A.: the right ground support for the best result in the

Use of Analytical Tools to Optimize Ground Operations and Processing


Flow Model: Utilizing Discrete Event Simulation for Future

Exploitation of the Soyuz launch pad in French Guiana

Maintenance & exploitation

Statistical Methods for the evaluation of the quality of measurement data on the

10h00 O37 - Modification of the DLR High Pressure Test Facility P3.2 to perform hot fire tests

of Stage Combustion Rocket Engines o

Volker Kraft

DLR German Aerospace Center


11h00 O38 - Operation of Test Facilities for Upper Stage Engines:

P4

Christopher

German Aerospace Center (DLR)

11h30 O39 - Improvement on Rocket Engine Test Facility concerning Maintenance and

Operation

Yohei Ogawa

JAXA, Miyagi,

12h00 O40 - Design and

Ground Test Facility

Philipp Kallina


12h00-14h00 The lunch is spons


stations

Chairs: Françoise Perrel and Jacques Gigou

14h00 O41 – STFO (Optical fiber transmission system for satellite):

for A6 / ELA4

Nicolas Hugues

CNES, Toulouse

14h30 O42 - Launcher Tracking Support from ESTRACK

Gerhard Billig

ESA, Darmstadt

15h00 O43 - Mobile Telemetry stations concept for launcher tracking

Bruno Masson

Telespazio France

Modification of the DLR High Pressure Test Facility P3.2 to perform hot fire tests

of Stage Combustion Rocket Engines on Pre-Burner and Main

Kraft

DLR German Aerospace Center, Hardthausen, Germany


Operation of Test Facilities for Upper Stage Engines: High Altitude Test Facility

Christopher Gusinde

German Aerospace Center (DLR), Hardthausen, Germany

Improvement on Rocket Engine Test Facility concerning Maintenance and

Ogawa

Miyagi, Japan

Design and Testing of Water Based Rocket Engine Exhaust Acoustic Absorber on

Ground Test Facility

Kallina


The lunch is sponsored by Telespazio.

Launch Range Facilities - Session 3 - communications

Jacques Gigou

STFO (Optical fiber transmission system for satellite):

for A6 / ELA4

Hugues

Toulouse, France

Launcher Tracking Support from ESTRACK

Billig

Darmstadt, Germany

Mobile Telemetry stations concept for launcher tracking

Masson

Telespazio France, Kourou, French Guiana

7

Modification of the DLR High Pressure Test Facility P3.2 to perform hot fire tests

Burner and Main-Chamber level


High Altitude Test Facility

Improvement on Rocket Engine Test Facility concerning Maintenance and

Testing of Water Based Rocket Engine Exhaust Acoustic Absorber on

communications - tracking

STFO (Optical fiber transmission system for satellite): Objective and evolution

Mobile Telemetry stations concept for launcher tracking


16h00 O44 - European Tracking Stations Networks Evolutions from Xmas 1979 to now

Michel Starozinski

CNES, Toulouse

16h30 O45 - Meteorological Data Analysis

Operation

BongJae Kuk

Korea Aerospace Research Institute

17h00 O46 - Introduction into Ground Telemetry System of Naro Space Center and Operation

Results at KSLV

Sun-Ik Lee

KARI (Korea Aerospace Research Institute)


Chairs: Jacques Bertrand and Christian Lardot

14h00 O47 - Optimization costs by mutualisation of chilled and hot

Serge Sellerian

CNES, Toulouse

14h30 O48 - Air liquide involvement in launch pad ground / launcher interfaces

François Barbier

Air Liquide Advanced Technologies

15h00 O49 - Soyouz Launch Complex

Pierre Guilhem

CNES, Toulouse


16h00 O50 - Twin screw mixer & continuous process

Yann Talamoni

Herakles (Safran Group)

16h30 O51 - “Historic and state of the art: the lightning protections of the space launch pads

on the Guyana Space Center (ARIANE 5, VEGA, SOYOUZ)”

Philippe Curot

CNES - Launchers Directorate


European Tracking Stations Networks Evolutions from Xmas 1979 to now

Starozinski

Toulouse, France

Meteorological Data Analysis and Strategy of Collaboration for NARO Launch

Kuk

Korea Aerospace Research Institute, Goheung, South Korea

Introduction into Ground Telemetry System of Naro Space Center and Operation

Results at KSLV-I Launch Mission

KARI (Korea Aerospace Research Institute), Goheung-gun, South Korea

Launch Complex - Session 3 - Specific Technical aspects

Christian Lardot

ptimization costs by mutualisation of chilled and hot

Sellerian

Toulouse, France

Air liquide involvement in launch pad ground / launcher interfaces

Barbier

Air Liquide Advanced Technologies, Sassenage, France

Soyouz Launch Complex Infrastructures

Guilhem

Toulouse, France


Twin screw mixer & continuous process - A credible solution for solid propulsion

Talamoni

Herakles (Safran Group), Le Haillan, France

“Historic and state of the art: the lightning protections of the space launch pads

on the Guyana Space Center (ARIANE 5, VEGA, SOYOUZ)”

Curot

Launchers Directorate, Toulouse, France

8


European Tracking Stations Networks Evolutions from Xmas 1979 to now

and Strategy of Collaboration for NARO Launch

Introduction into Ground Telemetry System of Naro Space Center and Operation

South Korea

Specific Technical aspects

ptimization costs by mutualisation of chilled and hot water production system

Air liquide involvement in launch pad ground / launcher interfaces


A credible solution for solid propulsion

“Historic and state of the art: the lightning protections of the space launch pads

17h00 O52 - Launch Pad Acoustic Suppression System for next generation Rocket Boosters

Singari Reddeiah

Indian Space Research Organisation(ISRO)


Chairs: Jacques Tanguy and Frédéric Munos

14h00 O53 - SOWARLA, Solar Assisted Water Treatment, DLR test centre Lampoldshausen

Andreas Haberzettl

DLR, German Aerospace Center

14h30 O54 - Evaluation of numerical bus systems used in rocket engine

Volker Schmidt


15h00 O55 - The experimental platform FAST: Facilities for Aerothermodynamics &

Supersonic Technologies

Viviana Lago

Laboratoire ICARE, CNRS


16h00 O56 - Cryo-laboratories for test and development of propellant storage and

management technologies

Jens Gerstmann

German Aerospace Center

16h30 O56 - Cryo Upper Stage Tank Demonstrator

Jörg Klatte

Astrium GmbH

17h00 O57 - Research On Launch Vehicle Test And Virtual Launch System Based On Model

Linna Wang

China academy of launch vehicle

19h00-23h00 The dining cocktail

Launch Pad Acoustic Suppression System for next generation Rocket Boosters

Reddeiah

Indian Space Research Organisation(ISRO), Sriharikota, India

Test Facilities - Session 3 - Sub systems & techniques

Frédéric Munos

SOWARLA, Solar Assisted Water Treatment, DLR test centre Lampoldshausen

Haberzettl

DLR, German Aerospace Center, Hardthausen, Germany

Evaluation of numerical bus systems used in rocket engine

Schmidt


The experimental platform FAST: Facilities for Aerothermodynamics &

Supersonic Technologies

Lago

Laboratoire ICARE, CNRS, Orléans, France

coffee breaks are sponsored by Telematic Solutions Advanced.

laboratories for test and development of propellant storage and

management technologies

Gerstmann

German Aerospace Center - Institute of Space Systems, Bremen, Germany

Cryo Upper Stage Tank Demonstrator

Astrium GmbH, Bremen, Germany

Research On Launch Vehicle Test And Virtual Launch System Based On Model

Wang

China academy of launch vehicle technology R&D center, Beijing, China

The dining cocktail is sponsored by Arianespace

9

Launch Pad Acoustic Suppression System for next generation Rocket Boosters

Sub systems & techniques

SOWARLA, Solar Assisted Water Treatment, DLR test centre Lampoldshausen

Evaluation of numerical bus systems used in rocket engine test facilities

The experimental platform FAST: Facilities for Aerothermodynamics &

coffee breaks are sponsored by Telematic Solutions Advanced.

laboratories for test and development of propellant storage and

Germany

Research On Launch Vehicle Test And Virtual Launch System Based On Model

China

is sponsored by Arianespace.

10

Friday 14 June 2013



O58 – Presentation of the French Guiana launch complexes

Jacques Bertrand

CNES, Toulouse, France

O59 - Reconsideration and conception of H-IIA, H-IIB and next generation facilities

Isao Kotani

Japan Aerospace Exploration Agency, Ibaraki-ken, Japan

O60 - Term Prediction of Vostochny Cosmodrome Development in Support of Space Activity

Alla Serikova

Central Research Institute of Machine Building (FSUE/TSNIIMASH), Korolev, Moscow region, Russia

11h00-11h30 Closing

11

POSTER EXHIBTION

Launch Range Facilities -

P01 - Low Profile and High Gain Yagi Wire-Patch Antenna for TT&C Applications

Hongjiang Zhang


P02 - An Analysis of the Design Requirements of General Assembly-test Building at Large Manned

Spacecraft Launch Site

Zhao Ting


P03 - Environmental protection technology of Satellite-rocket horizontally docking

Zhenyu Wu

Beijing Institute of Aerospace Systems Engineering, Beijing, China

P04 - Design of a Class of Communication Network of Drive Control System of Movable Launch

Platform

Daoping Li

Beijing Institute of Space Launch Technology, Beijing, China

P05 - Reliability Availability and Maintanability (RAM) of Earth Storable Propellant storages in Launch

pad

Karthigai Selvam

ISRO, Sriharikota, India

P06 - SOYUZ IATR (Integrated & Active TM Repeater)

Benoit RATTI

CNES, Toulouse, France

P07 - The Research of Spacecraft Automatic Test System

Xiaojun Liu

Research & Development of China Academy of Vehicle Technology, Beijing, China

P08 - Earth Based Sensors for Man-made Objects Navigation Solutions and Security of Space Assets

Andris Treijs

HEE Photonic Labs, Riga, Latvia

Launch Complex

P09 - The Method and Development of The Launch Vehicle Verticality Adjustmeng

Wu Mengqiang

Beijing Institute of Space Launch Technology, Beijing, China

P10 - Storable propellants : risks and stakes

Bruno Nicolas

VINCI Energies, Saint Denis, France

12

Test Facilities

P11 - Computer security in context of test bench risk management

Volker Schmidt


P12 - Validation and Qualification of a new test facility

Peter Lutz

ESA, Paris, France

Documents

PRELIMINARY PROGRAMME - Aventri...Detailed programme: Wednesday 12 June 2013 8h30-9h30 Opening Welcome addresses Michel Eymard, CNES, Paris, France 9h30-10h30 Plenary session 1 Chairs: