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Space tech Bremen, 24 October 2017 REUSABILITY VERSUS COST EFFICIENCY

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Page 1: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

Space tech Bremen, 24 October 2017

REUSABILITY VERSUS COST EFFICIENCY

Page 2: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

11

SUBSIDIARIES& MAIN AFFILIATES

€3 BILLION

ESTIMATED PRO FORMA SALES

9,000

EMPLOYEESIN FRANCE

& GERMANY

50/50

JOINT COMPANY BETWEEN

AIRBUS & SAFRAN

WORLD LEADER IN ACCESS TO SPACE

CIVIL

LAUNCHERS

Ariane 5

Ariane 6

Launch services

DEFENSE M51 program

EQUIPMENT

& SERVICES

For satellites, spacecraft

For launchers

For defence, security, critical

infrastructures and industry

31/10/2017

Page 3: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

LOCATIONS

FRANCE GERMANY

LES MUREAUX

VERNON

VERT-LE-PETIT

* Secondment to the French Navy site on Île Longue

** Locations on the Guiana Space Centre (CSG)

BREST*

LE HAILLAN

SAINT MÉDARD CENTRESAINT MÉDARD ISSAC

TOULOUSE

KOUROU**

BREMEN

LAMPOLDSHAUSEN

OTTOBRUNN

TRAUEN

APPKlundert (Netherlands)

ArianespaceKourou (France), Evry

(France), Washington DC

(United States),

Singapore, Tokyo (Japan)

CilasOrléans, Mont Audouze,

Le Barp, Aubagne (France)

EurockotBremen (Germany)

NuclétudesLes Ulis (France)

PyroallianceLes Mureaux, Toulon

(France)

SodernLimeil-Brévannes

(France)

SUBSIDIARIES AFFILIATES

EuropropulsionSuresnes, Kourou (France)

StarsemEvry (France)

RegulusKourou (France)

Euro Cryospace Les Mureaux (France)

31/10/2017

Page 4: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

ARIANE 5THE BENCHMARK

600EUROPEAN COMPANIES CONTRIBUTE

TO ARIANE 5

UNINTERRUPTED SUCCESS SINCE

2003

UP TO 10.5 tPAYLOAD TO GEOSTATIONARY TRANSFER

ORBIT (GTO)

© E

SA

-CN

ES

-AR

IAN

ES

PA

CE

/Optique V

idéo d

u C

SG

Its track record shows that Ariane 5 is the

world’s most reliable launcher

Ariane 5 ECA can lift more than 10 metric

tons into geostationary transfer orbit. Year

after year, it retains its position as the world’s

number one for orbiting telecommunications

satellites

Ariane 5 ES is the ideal solution for launching

missions to low- or medium-Earth orbit, such

as services for the International Space Station

(ISS) or deployment of the Galileo

constellation

31/10/2017

Page 5: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

ARIANE 5A FLEXIBLE, SCALABLE SYSTEM

ARIANE 5 ECA PERFORMANCE

GTO 9.9 t to 10.5 t

SSO > 10 t

LEO 20.6 t

31/10/2017

Page 6: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

ARIANE 6ALL COMMERCIAL AND INSTITUTIONAL MISSIONS

ARIANE 64 PERFORMANCE

GTO

10.5 to 12 t

MEO

SSO

LEO 20 t

31/10/2017

Page 7: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

ARIANE 6UNPRECEDENTED FLEXIBILITY, MODULARITY AND COMPETITIVENESS

ARIANE 64

(4 BOOSTERS)

Performance

12 t GTO

Launch weight 850 t

Thrust 1,500 t

ARIANE 62

(2 BOOSTERS)

Performance

4.5 t GTO

Launch weight 500 t

Thrust 800 t

Fairing

Height: 14 or 20 m

Ø 5.4 m

Dual launch system

Ø 4.5 m useful

Reignitable Vinci engine

Thrust: 18 t

2 or 4 P120 boosters

(common with Vega-C)

Thrust: 350 t

Vulcain 2.1 engine

Thrust: 137 t

31/10/2017

Page 8: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

Netherlands

Norway

Romania

Spain

Sweden

Switzerland

ARIANE 6INNOVATION AND RELIABILITY

UP TO

12 tPAYLOAD TO

GEOSTATIONARY TRANSFER ORBIT

(GTO)

13EUROPEANCOUNTRIESINVOLVED

2 OR 4BOOSTERS

FIRST FLIGHT

2020

Unprecedented flexibility

● 1 launcher, 2 versions: Ariane 62 and 64

● 2 types of fairings and numerous

configurations

● For launching all types of satellites

to all orbits

Maximum industrial efficiency

● Reduced production costs for greater

competitiveness

● End to end optimization: from “raw material”

to launch!UP TO

12LAUNCHES PER

YEAR

Austria

Belgium

Czech Rep.

France

Germany

Ireland

Italy

31/10/2017

Page 9: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

ARIANE 6A EUROPEAN INDUSTRIAL NETWORK ORGANISED INTOCLUSTERS OF EXCELLENCE

LAUNCH SYSTEM AND FINAL

INTEGRATION

ArianeGroup

BOOSTERS

ArianeGroup / Avio

via Europropulsion / Regulus

CRYOGENIC SYSTEMS

Air LiquideMETAL AEROSTRUCTURES

MT-Aerospace

Airbus DS Netherlands

COMPOSITE

AEROSTRUCTURES

Airbus DS (CASA)

FAIRING

RUAG

MECHANICAL GROUND

EQUIPMENT

APCO

THRUST

VECTOR CONTROLS

SABCA

31/10/2017

Page 10: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. --

TECHNICAL INNOVATION AT WORK: INNOVATING PAYS BACK

24/10/2017 10

PF52 horizontal test bed

Augmented realityFriction/stir welding (FSW) Lean manufacturing - V-line

3D printing

Page 11: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

EXPERTISE IN THE MOST ADVANCED CRITICAL TECHNOLOGIES

SOLID

PROPELLANT

LIQUID

PROPELLANT

ENERGETIC

MATERIALS

INTEGRATIONCOMPOSITE

MATERIALS

SYSTEM

DESIGN

31/10/2017

Page 12: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

GETTING READY FOR THE FUTUREOR EXPANDABLE, WE WILL ENABLE EUROPEAN ACCESS TO SPACE

31/10/2017

Reusable or expandable, we will enable European access to spacesable

Page 13: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

PROMETHEUS REUSABLE ENGINE IN DEVELOPMENT

31/10/2017

- Prometheus essential to

enhance competitiveness of

future European launchers

- Studies launched in 2015

(CNES contract) validated the

project’s credibility

- Development contract signed

with ESA in June 2017

The potential evolution of ARIANE 6 can include very

low cost liquid modules

Page 14: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED.

PROMETHEUS: ESSENTIAL TECHNOLOGIES FOR COST REDUCTIONS

31/10/2017

€10M €1M

TODAY TOMORROW

VULCAIN 2.1:

LH2-LOX

PROMETHEUS:

LOX-METHANE

Page 15: REUSABILITY VERSUS COST EFFICIENCY · Reignitable Vinci engine Thrust: 18 t 2 or 4 P120 boosters (common with Vega-C) Thrust: 350 t Vulcain 2.1 engine Thrust: 137 t 31/10/2017. THIS

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. -

THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP.

IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S

WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. 31/10/2017