JUICE Industry Day - emits.sso.esa.intemits.sso.esa.int/emits-doc/ESTEC/JUICE-Industry-Day-booklet_v2.pdf · JUICE Industry Day ... magnetosphere, and of the meteorology, chemistry

JUICE Industry Day

“Exploring the emergence of habitable worlds around gas giants”

Organised by ESA and Airbus Defence and Space SAS

27-28 October 2015

European Space Research and Technology Centre (ESTEC) Keplerlaan 1

2200 AG Noordwijk

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JUICE Industry Day

27 – 28 October 2015

European Space Research and Technology Centre (ESTEC)

Keplerlaan 1

2200 AG Noordwijk (The Netherlands)

Foreword 1. The JUICE Mission The JUICE spacecraft will provide a thorough investigation of the Jupiter system in all its complexity with emphasis on the three potentially ocean-bearing Galilean satellites, Ganymede, Europa and Callisto, and their potential habitability. JUICE has been tailored to observe all the main components of the Jupiter system and to disentangle their complex interactions. Central to this system, the Galilean satellites, span a broad range of possible internal structures that can be subdivided into two categories: two dominantly rocky (silicate/metal) satellites (Io and Europa) and two dominantly icy ones (Ganymede and Callisto). In order to place Ganymede, Europa and Callisto into the right context, and to better understand the Galilean satellites as a system, JUICE will conduct a comparative study of Ganymede, Callisto and Europa, with a special focus on Ganymede, which JUICE will characterise in great detail. The JUICE spacecraft will carry the most powerful remote sensing, geophysical, and in situ payload complement ever flown to the outer Solar System. The payload consists of 10 state-of-the-art instruments plus one experiment that uses the spacecraft telecommunication system with ground-based instruments. This payload suite is capable of addressing all of the mission's science goals, from in situ measurements of Jupiter's atmosphere and plasma environment, to remote observations of the surface and interior of the three icy moons, Ganymede, Europa and Callisto. It will provide a complete spatio-temporal characterisation of the giant, rotating magnetosphere, and of the meteorology, chemistry and structure of Jupiter's gaseous atmosphere. It will study the coupling processes inside the Jupiter system, with emphasis on (a) gravitational coupling, which ties together Jupiter and its satellite system, and (b) electrodynamics interactions, which couple Jupiter and its satellites to its atmosphere, magnetosphere and magneto disc.

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The spacecraft is planned for launch in 2022 and is foreseen to perform a 7.4 year cruise toward Jupiter, based on Earth-Venus-Earth-Mars-Earth gravity assists. The Jupiter orbit insertion will be performed in October 2029, and will be followed by a tour in the Jupiter system, including several flybys of Callisto, two Europa flybys, a phase in which a Callisto gravity assist sequence will be used to raise the orbit inclination in order to observe Jupiter’s polar regions and a transfer to Ganymede. In August 2032 the spacecraft will be inserted into polar orbits around Ganymede, starting with elliptical and high altitude (5000 km) circular orbits followed by a final phase with a 500 km circular orbit. 2. Responsibility The JUICE mission has been approved by ESA and delegated bodies for a planned launch in 2022 in the frame of the Cosmic Vision 2015-2025 plan. ESA has the overall responsibility for the JUICE mission design and implementation including the procurement of the launch service, with payload contributions from the ESA Member States. The industrial Prime Contractor is responsible for the procurement, development, manufacturing, assembly, integration (including the Instruments provided by the Member States), test, verification and timely delivery of a fully integrated spacecraft fulfilling the mission objectives. 3. The Industry Day Further to the Invitation To Tender (ITT) released by the European Space Agency (ESA) in December 2014, Airbus Defence and Space SAS has been appointed as Prime Contractor of the JUICE space segment for the Implementation phase (B2/C/D/E1). Therefore Airbus has been authorized to proceed with the competitive procurement process in order to complete the build-up of the spacecraft industrial team for spacecraft related items. This tendering process will be governed by ESA rules which are reported in the “Best practices for the selection of subcontractors by Prime Contractors in the frame of ESA’s major procurements”. This document can be downloaded from EMITS (http://emits.sso.esa.int/ under “Reference Documentation” and “Administrative Documents”). In consideration of the limited launch periods and recurring launch opportunities in about yearly intervals, to secure the 2022 launch window, the procurement of schedule critical elements has started in May 2015, during the Prime tendering period. Therefore, in parallel to the current announcement on EMITS of the schedule critical items ITTs, the objective of this Industry Day is to present to the European industry the overall JUICE mission, the associated business opportunities, the bidding process and schedule for the build-up of the JUICE spacecraft industrial team. The morning of the first day (27 October) will consist of presentations by ESA and Airbus about the JUICE mission and the various procurement opportunities. The procurement of electronic, electrical, and electromechanical components has been set up through a CPPA agent (Alter, Spain).

http://emits.sso.esa.int/

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This will coordinate orders with the objective of harmonising and standardising components, thus minimising cost, and meeting the applicable quality requirements. The afternoon of the first day (27 October) and the second day (28 October) will consist of face-to-face sessions for participants to present themselves and to discuss with ESA and Airbus. The duration of each session is limited to 20 minutes. It is foreseen to hold parallel sessions on the following subjects: 1. Mechanical, and Thermal ITTs 2. Propulsion ITTs 3. Mechanisms ITTs 4. Avionics, RF and Electrical ITTs 5. GSE, and Facilities ITTs 6. Software ITTs 7. System Support Activities ITTs 8. Programmatics The afternoon of the second day (28 October) will consist of meetings on the following special topics:

• Meeting with ESA • Meeting with Airbus • New Member States • German SMEs

Participants shall sign up for slots for the face-to-face sessions and the special topics meetings at the time of the registration to the event. The event will start at 09:30 on 27 October and will end no later than 17:30 on 28 October. JUICE Participating States For information, the Participating States in the JUICE Spacecraft implementation are: Austria, Belgium, the Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Ireland, Italy, Luxembourg, the Netherlands, Norway, Poland, Portugal, Romania, Spain, Sweden, Switzerland and the United Kingdom. Registration The registration is free of charge, however, for logistic reasons and in order to access ESA-ESTEC all participants will need to register in advance. Please indicate your participation by 21 October 2015, naming your company name and address, name(s) of participant(s), telephone number, e-mail address, your technical domain. You shall also register to the face-to-face sessions and special topic meetings you would like to attend.

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Please note that for logistic reasons the participation is limited to 250 people with a maximum of two (2) participants per Company. Please find additional information and register at the following link:

http://www.congrexprojects.com/15M69 The list of participating companies will be published by 22 October to allow companies to identify possible partners and have the opportunity to meet during the event. Contact for specific enquiries regarding agenda and contents ESA Conference Bureau P.O Box 299 2200 AG Noordwijk The Netherlands Phone: +31 71 565 5005 Fax: +31 71 565 5658 Email: [email protected]

http://www.congrexprojects.com/15M69

mailto:[email protected]

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Agenda

Day 1 Location: ESCAPE Tennis Hall 8:00 – 9:30 Registration 9:30 – 10:30 ESA Presentation

• Introduction : objectives & organization of the JUICE Industry Day • The JUICE mission, System and Space segment, Programmatics, Procurement

approach, GEO return constraints • CPPA (Coordinated Parts Procurement) • Use of ECOS

10:30 – 12.00 Airbus Presentation

• The JUICE Spacecraft, technical and development, models, objectives & schedule,

product tree and constituents • The ITT process (according to Best Practices) and ITT walk through

12:00 – 13:00 Face-to-face splinters (see further for details) 13:00 – 14:00 Lunch break 14:00 – 19:00 Face-to-face splinters (20 minutes each) Eight sets of parallel face-to-face splinter meetings:

1. Mechanical and Thermal ITTs 2. Propulsion ITTs 3. Mechanisms ITTs 4. Avionics, RF and Electrical ITTs (2 tables) 5. GSE, and Facilities ITTs (2 tables) 6. Software ITTs 7. System Support Activities ITTs 8. Programmatics

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Day 2 09:00 – 13:00 Face-to-face splinters Location: ESCAPE Tennis Hall Eight sets of parallel face-to-face splinter meetings :

1. Mechanical and Thermal ITTs 2. Propulsion ITTs 3. Mechanisms ITTs 4. Avionics, RF and Electrical ITTs (2 tables) 5. GSE, and Facilities ITTs (2 tables) 6. Software ITTs 7. System Support Activities ITTs 8. Programmatics

13:00 – 14:00 Lunch break 14:00 – 15:30 and 15:30 – 17:00 Special items group meetings (two sessions)

• Meeting with ESA * room Ba030 • Meeting with Airbus * room Ba024 • New Member States room Df121 • German SMEs room Ef008

*) These forums are dedicated to the participants to address topics, issues, concerns, propositions, regarding the JUICE mission, to ESA and Airbus, for open and free discussion.

14:00 - 17:00 Face-to-face splinters Four sets of parallel face-to-face splinter meetings:

1. Mechanical and Thermal ITTs 2. Avionics, RF and Electrical ITTs (2 tables) 3. GSE, and Facilities ITTs (2 tables) 4. Software ITTs

The Tennis Hall chairs will remain available for the participants until COB .

M. Baroni | JUICE_Introduction_for_Industry_Day| Slide 1

JUICE Industry day

M. Baroni ESA / JUICE Project Control & Admin Manager

27 -28 October 2015


ESA and Airbus Defence & Space welcome the participants to the JUICE Industry Day

o 232 participants o 173 companies o 22 countries

Introduction


Forewords and Objectives

o To present: o the overall JUICE mission o the bidding process and schedule o the associated business opportunities

o Opportunity for presenting your company experience and potential

o Opportunity for addressing issues, questions, concerns

o Opportunity for meeting possible partners


Agenda – Tuesday 27th October

09:30 – 10:30 ESA Presentation ESCAPE Tennis Hall 10:30 – 12.00 Airbus Presentation 12:00 – 13:00 Face-to-face splinters 13:00 – 14:00 Lunch break 14:00 – 19:00 Face-to-face splinters (20 minutes each)

• Mechanical and Thermal ITTs • Propulsion ITTs • Mechanisms ITTs • Avionics, RF and Electrical ITTs (2 tables) • GSE, and Facilities ITTs (2 tables) • Software ITTs • System Support Activities ITTs • Programmatics


Agenda – Tuesday 28th October

09:00 – 13:00 Face-to-face splinters (ESCAPE Tennis Hall) 13:00 – 14:00 Lunch break 14:00 – 15:30 and 15:30 – 17:00 Special items group meetings • Meeting with ESA (room Ba030) • Meeting with Airbus (room Ba024) • New Member States (room Df121) • German SMEs (room Ef008)

14:00 - 17:00 Face-to-face splinters (ESCAPE Tennis Hall)

JUICE Industry Day 27—28 October 2015 ESA/ESTEC

Restaurant

Escape Building

Security Gate

Walking from Escape to Ba030 (Mee ng with ESA)

Walking from Escape to Ba024 (Mee ng with Airbus)

Walking from Escape to Df121 (New Member States)

Walking from Escape to Ef008 (German SMEs)

Corridor Ef

Corridor Df Corridor Ba

JUICE Industry Day

G. Sarri – ESA / JUICE Project Manager

27th October 2015

G. Sarri| JUICE_programme_status_for_Industry_1| Slide 2

JUICE : Jupiter Icy Moons Explorer


Scientific Objectives (1/3)






Overall Mission Profile

Launch 1st June 2022

Interplanetary transfer 7.4 years

Jupiter Orbit Insertion October 2029

2 Europa flybys October 2030

Jupiter high-latitude phase & Callisto flybys December 2030 – May 2031

Transfer to Ganymede June 2031 - July 2032

Ganymede Orbit Insertion August 2032

Ganymede elliptical orbit / 5000 km circular orbit August – December 2032

Ganymede 500 km circular orbit January – June 2033

End of Mission June 2033


Trajectory for cruise phase


Trajectory for cruise phase

Trajectory for cruise phase : animation


Elements of the JUICE program

Ground Stations: Cebreros New Norcia Malargue

Mission Operation Centre (MOC)

ESOC

Science Operation Centre (SOC)

ESAC

Launcher:Ariane 5 ECA

European ScienceCommunity (with PI

provided instruments)

Spacecraft:Airbus D&S SAS


Prime Contractor selection

Airbus Defence & Space SAS has been selected as the JUICE Prime Contractor

294th IPC meeting on 16th July 2015, ESA/IPC(2015)87 Phases B2, C/D and E1 kicked-off on 28th July 2015.

Consortium

Core Team Airbus D&S SAS (FR) Project Office/ CSW / Spacecraft EM AIT Airbus D&S GmbH (DE) Electrical System / Spacecraft PFM AIT Airbus D&S Ltd (UK) Mission Analysis Support Vectronic (DE) Mission Simulator NMS (RO, CZ, PL) OPS & DB / Structural Analysis / CSW support

Best Practices to complete the consortium by mid 2017 87 procurements to be performed Includes 6 Subsystems


Spacecraft configuration (1/2)

Main resources

Mass Dry ≈ 2200 kg Propellant ≈ 2900 kg Total > 5000 kg Instruments: 218 kg

Power Total < 1000 W Instruments GCO500 =180 W Instruments fly-by = 230 W (360 W for ½ h)

Memory = 1 Tbit EOL (CDMS requirement) ∆v ≈ 2700 m/s Data Rate: 1.4 Gb/24 h


Spacecraft configuration (2/2)


Summary of Instruments

Instrument Name Principal Investigator Instrument Key Elements Instrument Type & Key Properties

Rem

ote

Sen

sin

g

Jovis, Amorum ac Natorum UndiqueScrutator (JANUS) P. Palumbo (IT)

OH (Optical Head)PEU (Proximity Electronic Unit)MEU (Main Electronic Unit)

Imaging system350 – 1050 nm, 13 filters;FOV: 1.72x1.29°,up to 3 m/px (moons)up to 15 km/px (Jupiter)

Moons And Jupiter Imaging Spectrometer (MAJIS)

Y. Langevin (FR),G. Piccioni (IT)

OH (Optical Head)PE (Proximity Electronic)MEU (Main Electronic Unit)

Vis-Near IR imaging spectrometer0.4 – 5.7 µm, resolution 3 – 7 nm; FOV: 3.4°, up to 0.025 km/px (moons),125 km/px (Jupiter)

UV Spectrograph (UVS) R. Gladstone (US) Single unit55 – 210 nm, resolution <0.6 nm; up to 0.5 km/px (moons),250 km/px (Jupiter)

Sub-mm Wave Instrument (SWI) P. Hartogh (DE)TRU (Telescope and Receiver Unit)EU (Electronic Unit)Rad (Radiator)

530-625 GHz (500 µm), resolving power 107; 30 cm antenna, resolution 1 – 2 mrad

Geo

ph

ysic

s

GAnymede Laser Altimeter (GALA) H. Hussmann (DE)TRU (Transmitter Receiver Unit)LEU (Laser Electronic Unit)ELU (Electronic Unit)

30 Hz shot frequency, resolution up to 50 m horizontal, 0.1 m vertical

Radar for Icy Moons Exploration (RIME) L. Bruzzone (IT)RDS (Receive and Digital Subsystem)TX (Transmitter)MN (Matching Network)

Ice penetrating radar9 MHz (1&3 MHz bands)16 m antenna; up to 9 km depth, 50-140 m resolution in ice

Gravity & Geophysics of Jupiter and Galilean Moons (3GM) L. Iess (IT) KaT (Ka Transponder)

USO (Ultra Stable Oscillator)

Radio-science experimentGravity field up to degree 10 at Ganymede; Structure of the Jupiter atmosphere 0.1 –800 mbar

In s

itu

Par

ticl

es a

nd

Fie

lds JUICE Magnetometer (J-MAG) M. Dougherty (UK)

MAGOBS (Outboard Sensor)MAGIBS (Inboard Sensor)MAGSCA (Scalar Sensor)MAGELB (Electronic Box)

Rates: 32 & 128 Hz±8 µT with ∆B = 1 pT±50 µT with ∆B = 6 pT

Particle Environment Package (PEP) S. Barabash (SE)ZU (Zenith Unit), NU (Nadir Unit),

Plasma environment package6 sensors; neutrals, ions, electrons; energy range <0.001 eV to >1 MeVcomposition with mass range 1 – 1000 amuand M/dM > 1100

Radio & Plasma Wave Investigation (RPWI) J.-E. Wahlund (SE)SCM (Search Coil Magnetometer)4 x LP (Langmuir Probe)RWI (Radio Wave instrument)EBOX (Electronic box)

6 sensors (4 LP, 1 SCM, 1 RWI antenna)E-field : DC – 45 MHz,B-field : 0.1 Hz – 20 kHz;plasma properties: Ne, Ni, Te,Vi ; dustcharacterisation (>1 µm)


Master Schedule


JUICE procurement approach

The JUICE procurement was approved by IPC: ESA/IPC(2014)1, add 47, rev1, Paris, 26 January 2015

All activities to be subcontracted will be procured following the ESA Code of best Practice (ESA/IPC(2012)65, rev2)

In principle, two steps: The Prime Contractor will select the subsystems responsible (6 subsystems),

including allocations for the equipment belonging to it The selected Subsystem Contractor will select the equipment responsible

Other equipment will be directly selected by the Prime Contractor

The procurement plan is regularly reviewed and adapted in order to achieve the geographic return requirements.

In doing so, preferential clauses, limitations, restricted competitions or direct negotiation may be used.

For stringent technical and programmatic reasons, the competition may be enlarged to non-Member States.


Planned procurements

6 Subsystems

SSTS (Structure Shielding and Thermal Subsystem)

CPS (Chemical Propulsion Subsystem)

SGS (Solar Generator Subsystem)

EPS (Electrical Power Subsystem)

CDMS (Central Data Management System)

COMS (Communication Subsystem)


GEO return requirements

Member State Return Requirements [%]

Return Requirements[M€]

Austria 2.8 8.5

Belgium 3.2 9.7

Czech Rep. 1.2 3.6

Denmark 2.3 7.0

Finland 1.7 5.1

Greece 1.9 5.8

Ireland 1.3 3.9

Luxembourg 0.2 0.6

Netherlands 4.6 13.9

Norway 3.6 10.9

Poland 3.2 9.7

Portugal 1.5 4.5

Romania 1.1 3.3

Spain 7.9 23.9

Sweden 3.6 10.9

Switzerland 4.9 14.9

Sub-total 45 136.2

France

55 166.4GermanyItalyU. Kingdom

Total 100 302.6 (Weighted value)

ECOS – The ESA Costing Software

ESA UNCLASSIFIED – For Official Use

Carla Signorini | ESTEC | 15/09/2011 | Slide 2

ECOS benefits

1. ECOS 5.1 unanimously welcomed by the ESA bidders’ Community 2. Allows error-free Price aggregation 3. Faster than Excel-based spread sheets once configured 4. All PSS-A forms printed in one batch and many more.



ECOS - The Rate File

Rate file noticeable features

Escalation tables

Variable rate agreement

Multiple

Overheads and Profit rates

Average sellable

hours/year




ECOS - Building the PT/WBS with Support Functions


The Turbo Data entry

1. Allows to perform Data entry from Excel if preferred

2. Allow to import data from ERP system

3. Several Excel templates available



Travel Plan

1. Drag’n drop from Travel Library allows very fast Travel Plan elaboration 2. Travel Plan table produced as Exhibit B to PSS-A2 report




ECOS - The Price Data Entry Summary

1. Allows to check totals and visualise price details for a. Own-share b. Budgetary sub-cos active provisions c. Budgetary sub-cos replaced by integrated Tender files



ECOS - The Integration window

1. Allows to : a. visualise received offers from sub-contractors b. Select retained offers from sub-contractors c. Calculate overall price on this basis



ECOS - The Payment Plan Data Entry

1. Real time comparison between cumulated expenses and milestones cumulated payments as the payment plan is being built

2. Direct Payment by ESA can be taken into account

3. Report 5405 produces the Payment Plan



ECOS - A global view over the price


ECOS - Advanced features


Advanced features Comments

Price rounding To give an elegant final touch to the price by presenting rounded numbers per phase. Rounding can easily be cancelled if and when price has to be reworked before generating/submitting the tender

Time shifting To recalculate instantly expenses profiles and escalation in FFP for the block of activities concerned (totality of the scope or only a WBS branch

Fully supported yearly variable rates

To automatically calculate yearly amounts when variable yearly rates apply to some resources categories, overheads or profit rates. Recalculations in case of time shifting are instantaneous

User WP numbering The User can define his own WP numbering system and visualize WP list summaries and produce all WP-related reports sorted by User numbers

Product Libraries

To record and later reuse by simple drag’n drop, blocks of WBS including resources for any type of product. Highly recommended for Equipment suppliers. Also suitable for standard sets of Project Office activities. Allows to transfer all data entries from one file to another in case of data recovery or any kind of contingency action. For instance: transferring all data entries entered in own created project file into an ITT file received from the Upper-tier contractor at a late stage

Travel Libraries All elementary records of price per trip/daily subsistence at your finger tip. Excel Imports (from finance department for instance) allowed

Import/Export dates Allow Import/Export to/from any planning tool (Excel based)

Import/Export data Allows Import/Export to/from any ERP system (CSV based)

Colour settings The User can define his set of colours for various mode (Maintenance/Data Entry/Tender). Useful and agreeable


ECOS - How to get and install ECOS ?

1. Contact the ECOS Help Desk: Tel: +31.(0)71.565.6500 Email: [email protected]

2. Self-Training and Quick Guidelines available from download on

EMITS :

3. ECOS Process description available at Industry Portal: http://www.esa.int/About_Us/Business_with_ESA/How_to_do/Submitting_an_ECOS_proposal



JUICE Industry Day

- Noordwijk, October 27/28th, 2015 -

‘ We make it flyby ’

JUI-ASFT-SYS-HO-024

Agenda

Programme status

Project Team organisation

Industrial organisation

Mission and spacecraft configuration

Verification logic and development schedule

Procurement approach

Main Tender Conditions

Questions / answers

3

Date - 4

JUICE programme environment and status

JUICE is the first L-Class mission of the ESA ‘Cosmic Vision’ programme

Airbus selected as Prime Contractor at IPC held on July, 16th 2015

ESA / Airbus negotiation successfully completed on July, 24th 2015

Kick-off with ESA held on July,28th 2015. This is 2 months ahead of the initial plan (ITT)

Fixed launch date on May, 20th 2022 ! “Time is of the essence”. Schedule adherence will be key. ESA and Airbus already putting strong pressure on the early

milestones of the Project.

Industrial consortium to be finalised within18 months, by PDR Schedule critical items already selected in the frame of Airbus proposal.

87 items to be selected under ESA Best Practices, including 6 subsystems.

Payload management 10 scientific instruments as CFI

However, Airbus fully committed to ensure the timely deliveries of the instruments (dedicated payload Airbus team)

4

Agenda

Programme status

Project and industrial organisation





Questions / answers

5

The Prime Project Team - A fully integrated joint team

6

Project Manager

Vincent Poinsignon

Instrument Team Manager

Xavier Moisson

Contract Officer

Christine Durand Schedule Control

Dominique de Bruyn

Project Control

Maité Aimé

Industrial Development

Expertise

Stephane Osipenco

Configuration Manager

Damien de Paysac

Technical Officers for the in-situ, radio and

radar instruments

PEP Uwe Kummer

RPWI Stephane Osipenco

JMAG Stephane Osipenco

3GM Michael Chwalla

RIME Uwe Kummer

Technical Officers for the optical instruments

SWI Jean Marc Goutoule

JANUS Xavier Moisson

MAJIS Benjamin Massart

UVS Benjamin Massart

GALA Michael Chwalla

Mission analysis Steve Kemble

Radiations Thierry Bouchet

Magnetic/EMC Markus Faust

Mechanical, Thermal & Propulsion Philippe Moinard

• Mechanical & Structure Sébastien Laborde

• Thermal Anthony Darel

• Mechanisms Charles Lambert

• Rime antenna & MAG boom Hans Joachim Schoedel

• Propulsion Philippe Moinard

• Solar Generator Didier Loche

Development, AIV and TDA

Thomas Schirmann System Engineering Manager

Frédéric Faye

Mission & System

performances

Cyril Cavel

Industrial Manager

Christian Lebranchu

AIT Manager

Philippe Durand

Deputy

Christophe Gabilan

Procurement

Coordination

Alain Tabouelle

EM AIT

Philippe Durand

PFM AIT

Thilo Nacke

FHN Local Project Manager

Markus Faust

Product Assurance Manager

Pierre Thoral

Satellite Design Authority Philippe Temporelli

Instruments Expert Gilles Planche

Avionics Philippe Humbert

• AOCS & Navigation Pascal Régnier

• FDIR, Operations & database Eric Ecale

• CDMS Philippe Humbert

• Software Luc maillet

• Functional Verification Frédéric Juillard

Electrical Helmut Gramatke

• Power Clemens Kalde

• RF Communications Robert Purvinskis

• Magnetic performance Klaus Bubeck

• EMC / RMC cleanliness John Aulton

Spacecraft architects

Subcontracts

Manon Bougy / Marion Hugues

Secretariat and Documentation

Lydie Pinel

JUICE Industrial Organisation

7

ESA

Airbus Defence and Space SAS (FR)JUICE Spacecraft Prime Contractor

· Project Office· AOCS and Central Software

· Spacecraft EM AIT

· Electrical system engineering· Instruments management support· Spacecraft PFM AIT

Airbus DS GmbH (DE)NMS Core Team Partners:

· Operations & Database support: CS Romania (RO)

· Structural Analyses support: Serenum (CZ)· Central Software development support:

Mobica (PL)

Structure, Shielding, Thermal

subsystem(SSTS)

SSTS equipment& services

Other Spacecraft Equipment & Services

Chemical Propulsion subsystem

(CPS)

Solar Generator subsystem

(SGS)

Electrical Power

subsystem(EPS)

Command & Data Management

subsystem(CDMS)

Communications subsystem

(COMS)

CPS equipment& services

SGS equipment & services

EPS equipment& services

CDMS equipment& services

COMS equipment& services

Central CylinderCASA Espacio (ES)

Propellant Tanks

To be selected

Spacecraft Interface Simulator (SIS)SSBV Rovsing (DK)

Best Practices

Pre-selected critical equipment

CPPA: Alter (ES)

Mission Analysis SupportAirbus DS Ltd (UK)

ESA selected contractors

RADEM: Efacec (PT)

Core Team

Mission Simulator: Vectronic (DE)

Co

re T

eam

Lay

erSu

bsy

stem

La

yer

Equ

ipm

ent

and

Ser

vice

s La

yer

Agenda

Programme status






Questions / answers

8

JUICE key figures

9

Mission

7,5 years cruise

3,5 years at Jupiter

More than 6 billion km travelled

10 scientific instruments

More than 2 Tbit of scientific data returned to Earth

Solar flux from 3,3 kW/m² (Venus flyby) to 50 W/m² at Jupiter

Radiation dose 10 times higher as a 15 years mission in GEO

Spacecraft

Largest solar arrays ever built (97 m²)

Delta-V : 2,4 km/s

Payload mass : 218 kg

Propellant mass : 2850 kg

Launch mass : 5250 kg

The JUICE spacecraft (1/3)

10


11


12

Functional architecture

13

Solar Generator Subsystem

Payload

Chemical

Propulsion

Subsystem

Command and Data

Management Subsystem

Attitude

and Orbit

Control

Electrical and Power

Subsystem


RF Distribution

Assembly

Antenna Pointing

Mechanism

Solar Array Drive

Electronics

High Gain

Antenna

Medium Gain

Antenna

Main Engine

MIL-STD-1553 B data bus

SpaceWire

Deployment

linesProtected

power

linesThermal

control

Star Tracker

Electronics

Sun Sensor

Star Tracker

Optical Head

Reaction Wheel

Star Tracker

Electronics

Sun Sensor

Star Tracker

Optical HeadStar Tracker

Optical Head

Reaction WheelReaction WheelReaction Wheel

Solar Array Drive

MechanismBattery

Power Control and

Distribution Unit

Deep Space

Transponder

Travelling Wave

Tube Amplifiers

(X-band, Ka-band)

Deep Space

Transponder

Ka-band

Travelling Wave

Tube Amplifier

Travelling Wave

Tube Amplifiers

(X-band, Ka-band)

X-band

Travelling Wave

Tube Amplifier

Datation pulse

JANUS GALA J-MAG RIME PEPSWI UVS MAJIS RPWI3GM RADEM

Antenna Pointing

Mechanism

Electronics

Command and

Data Management

Unit

Low Gain Antenna

Inertial

Measurement Unit

(including

accelerometers)

Navigation

Camera

Solar Array

Reaction Control

Thrusters

Remote Interface

Unit

JUICE Monitoring

Unit

JUICE Monitoring

Camera

. 64 Mhz on board central computer embedding a 1 Tbit mass memory

. X and Ka band communication. Science data telemetry from 1,4 Gbit to 3,9 Gbit per

day

. Enhanced on board monitoring: mini cameras and solar generator performance

control

Electrical architecture

14

. SpW interfaces for all instruments (but 3GM), with cross-strapping implemented in the

CDMS S/S.

. Regulated +28V bus supply to all PSUs (Nom + Red)

. Survival heaters and thermistances managed by the spacecraft

Electrical Power Subsystem

15

The EPS autonomously manages primary power control,

energy storage and bus voltage regulation. It is capable of

being powered by either the solar generator or the battery

or both at the same time, in-orbit as well as on ground.

The EPS architecture is based on a regulated 28Vdc

primary power bus (28V-BR) for single failure tolerant

primary and comprises:

• A Power Control and Distribution Unit (PCDU)

• a Lithium-Ion Battery Assembly consisting of five battery

modules

• the Solar Generator (SG) and its dedicated mechanisms

(HDRM),

• the Solar Array Drive Mechanisms (SADM),

• the Solar Array Drive Electronics (SADE)

The wiring harness, necessary to electrically interconnect

the spacecraft units, is procured separately.

Communication Subsystem and Antennas

16

The Communication Subsystem comprises the

following main components:

• The X / X, Ka-Band Deep Space Transponder

(DST) with TC uplink capability in X-Band, TM

downlink capability in X-/Ka-Band and support

of ranging and DDOR;

• The 52 W redundant X-Band Travelling Wave

Tube Amplifier (TWTA);

• The 27 W redundant Ka-Band TWTA;

• The RF Distribution Assembly (RFDA) to

interconnect the transponders and the 3 GM

instrument with the relevant antennas,

The antenna suite is composed of :

• A 2.4 m X-/Ka-Band High Gain Antenna (HGA)

for communication and 3GM support during

cruise, flybys and Ganymede orbits;

• An X-/Ka-Band Medium Gain Antenna (MGA)

for communication and 3GM support during

interplanetary cruise and contingency case at

Jupiter distance;

• Two X-Band Low Gain Antennas (LGA) for

quasi spherical coverage during LEOP and

emergency phases.

• The 3GM KaT and USO (part of payload

deliveries).

Control & Data Management Subsystem

17

Main features :

• High-performance processing core

• An On-Board Computer Mass Memory (OBC-MM)

capacity of 8 Gbit EOL.

• An integrated science mass memory

• Science mass memory compatible with the

simultaneous transmission of science data files to

the X-band and Ka-band, designed as an integrated

CDMU hardware/software function:

• Dedicated CDMU HW module for memory

resources and basic control logic, i.e. the Solid-

State Mass Memory

• Dedicated CSW components implement file

management as well as file downlink support

services.

• SpaceWire interfaces towards the instruments (but

3GM) for science data acquisition and towards the

processor (for mass memory control), with cross-

strapping implemented in the CDMS S/S.

• At SSMM module input, science data packets are

multiplexed onto 100 Mbps SpaceWire link(s).

• CFDP downlink implementation and management

concept

• Hardware-implemented CFDP engine that is

dedicated to downlinking the native science data files

through X- and/or Ka-band TM channels.

Thermal Control Concept

18

• Instruments survival heaters and thermistances

managed by the spacecraft

• The platform thermal control is based on well-known

and simple passive hardware such as heatpipes or MLI

Blankets.

• Most of the platform and instruments electronic units are

accommodated inside the vaults with the same -

20°C/+50°C design operating range. The link between

radiators and units is ensured thanks to a network of

surface heatpipes (or HPS) and embedded heatpipes (or

HPE)

• Low dissipative units are accommodated on the central

cylinder to limit vaults size and mass.

AOCS Functional Chain

19

Main features :

• High accuracy and autonomous star trackers:

three Optical Heads with large inter-head

angular separations to meet pointing

performance specifications with two heads

• High performance gyros for nominal and safe

modes with embedded accelerometers to meet

DV accuracy requirements

• High capacity reaction wheels to support the

high kinematics during Jovian moon flybys and

to store sufficient angular momentum to

minimize off loading frequency in Ganymede

orbit.

• A complete thruster configuration with pure

torque and longitudinal / transverse force

capability to support all kinds of ΔV

manoeuvres, with in addition the required main

engine controllability

• A narrow FOV Navigation Camera (NAVCAM) to

navigate around Jupiter;

• Two Sun sensors to ensure a safe Sun

Acquisition. One of the Sun sensor is used as

an Attitude Anomaly Detector during inner

cruise phases when the spacecraft Sun-pointed

attitude is thermally critical.

EMC requirements

20

Vaults and Harness are designed to ensure a maximum EMC

tightness External surfaces, including solar cells, are conductive

Magnetic cleanliness requirements

Magnetic disturbances on board JUICE constitue a threat on scientific performances

The only way forward to meet the specification consists in moving sensitive sensors away from the

spacecraft body

A 10.6 m MAG-Boom is therefore implemented on-board JUICE

This needs to be complemented by other precautions measures

material, internal accommodation and lay out, shielding

De-perming of equipment before delivery, and specific precautions during transportation and AIT at all levels

21

The JUICE S/C magnetic cleanliness shall enable :

• Discrimination of oceanic signals from icy moons, analysis of interactions between

magnetospheres of Jupiter and Ganymede,

• analyses of Europa and Callisto magnetic signatures induced by the Jovian

magnetic field

Robustness to radiations (1/2)

22

Accommodating the electronic equipment in the vaults allows to get the dose level on

parts below 50 krad at end of life (Ganymede circular orbit)

Rule of Thumb

o total dose of 2 Grad outside spacecraft, 1 Mrad inside the vaults and

50 krad inside electronics of vaults

o External harness has to withstand typically 10 Mrad.

Robustness to radiations (2/2)

23

The vaults allow to limit the radiations dose on the parts.

A local shielding is implemented for the parts which do not sustain 50 krad AND are

located in the worst areas in the equipment.

Agenda

Programme status






Questions / answers

24

Development Drivers

Launch on June, 1st 2022 3 weeks launch window,

Shortest interplanetary transfer to Jupiter (7.4 years),

6 months schedule reserve under ESA control.

A comprehensive verification plan Very stringent environment requirements (thermal, radiation, charging),

Very demanding performance requirements driven by scientific instruments (particularly EMC and magnetic

cleanliness requirements),

Flexibility for science instruments Late modifications of instrument interfaces up to 6 months after PDR,

Accommodation of staggered delivery of instruments Flight Models over a period of one year.

Mastering technology development JUICE mission specificities require adaptation of existing technologies (radiation environment, thermal environment,

use of solar cells under LILT conditions, complexity of Jupiter tour, large appendages),

A comprehensive Technology Development Activity (TDA) programme covering all these aspects is underway.

25

Development Logic, Phases and Reviews

26

Spacecraft PFM Integration and Qualification

Kick-Off SRR PDR CDR

PHASE B2 : Preliminary Definition

Phase PHASE C/D : Detailed Definition, Production and Verification Phase

System Requirements

ConsolidationPreliminary Design

Detailed Design and Performances Consolidation

(Budgets and Analysis / Review of Design)Performances Validation and Consolidation

Subsystem & Equipment Selection Process

Eqpt

Kick-Off

Eqpt

PDR

Eqpt

CDR

Equipment design

Equipment

Development &

Qualification

Flight Model

Acceptance

FAR

Subsystem & Equipment ITT

Preparation

Instruments Preliminary

Design

IPDR ICDR

Instruments Detailed Design

PHASE E1: Launch and

Commissioning Phase

NECR

Development Plan Consolidation

Early Thermal

Verification on TDM

Early Functional, EMC and Magnetic Verification on Spacecraft EM

IFDR

Instruments Manufacturing & Qualification

Instrument Interface Consolidation

S/S

Kick-Off

S/S

PDR

S/S

CDRS/S QR

Launch

Campaign

Spacecraft

Commissioning

Subsystem Preliminary DesignSubsystem Detailed

Design

Subsystem

Qualification

Eqpt

QR

Provision for Instruments

Staggered Delivery

Late Interface

Modification

ESA Technology Development Activities

Additional Technology Development Activities

Sp

ac

ec

raft

Le

ve

lIn

str

um

en

t

Le

ve

lS

ub

sy

ste

m &

Eq

uip

me

nt

Le

ve

lT

ec

hn

olo

gy

De

ve

lop

me

nt

In-flight

Performance

Verification

Model Philosophy

27

SVF

Early Mechanical

Verification

Early Functional, EMC

and Magnetic Verification

(AOCS) FAME

AOCS Performance

Verification

Eqpt./Inst.Qualification

Equip./

Instrument EQM

Static tests

Structure PFM

Heritage & Technology

Development Activities

Eqpt./Instr. Development

Equip./Instrument

EM

Equip./Instrument

Acceptance or Delta-

Qualification

Eqpt /

Instrument

PFM

Key

Hardware Flow

Development Logic Flow

System Level

S/S or Equipment Level

S/C PFM

Build acceptance

Mechanical & Thermal

Qualification

EMC Qualification

SVT with MOC

CDMU EBB

RF Suitcase

Ground Segment RFCT

CCS

Subset of Func. Verif.

Test Procedure

Real Time

Simulator

Software Verification

S/C EM

Complete Func. Verif.

Conducted EMC

AC Magnetic charac.

SVT with MOC

TRSP EM

Early Thermal

Verification

Thermal test

S/C TDM

Verification Levels within Industrial Chain

28

SGS

CPS

Prime Contractor

SSTS

EPS

PlatformEquipment

Scientific Instruments

CDMSCOMS

Technology Development Activities

Key

FM Flow

EM Flow

System Level

Subsystem level

Primary

Structure

SGS Qualification

and Acceptance

CPS Components

Qual. And

Acceptance

CPS Assembly on

S/C Structure

CPS Subsystem

Qual. And

Acceptance

Assembled

Structure/CPS

Structure Qual.

And Acceptance

Early Thermal

Verification on

TDM

MLI Qual. And

Acceptance

Battery

Qual. And

Accept.

PCDU

Qual. And

Accept.

EPS Subsystem Qual.

And Acceptance

Early Functional, EMC and

Magnetic Verification

on S/C EM

S/C PFM Qualification and

Acceptance

Secondary

Structure

S/C PFM Integration

Sensors &

Actuators Qual.

And Acceptance

Instrument

Qual. And

Acceptance

Early

Instrument

Interface

Verification

with SIS

CDMU

Qual. And

Accept.

RIU Qual.

And

Accept.

CDMS Subsystem Qual.

And Acceptance

TRSP

Qual. And

Accept.

COMS Subsystem Qual. And Acceptance

TWTA

Qual. And

Accept.

RFDA

Qual. And

Accept.

Central Software

Development

Antennas Qual.

And Acceptance

Instruments

Support HW Qual.

And Acceptance

RADEM Qual.

And Acceptance

Other Platform

Equipment Qual.

And Acceptance

Equipment level

Instrument level

ESA TDA’s

Industry TDA’s

EMs

FMs

Transportation Plan

Road transport from Friedrichshafen to

ESTEC Noordwijk (for environmental

test)

Road transport from ESTEC Noordwijk

to IABG Munich (for magnetic tests)

Road transport from IABG Munich to

Toulouse (for CPS leak test, final tests

and Solar Arrays integration)

Flight transport from Toulouse to

Kourou (launch campaign)

29

55AIRBUS DS

Friedrichshafen

IABGOttobrunn

ETSNoordwijk

AIRBUS DSToulouse

44

11

33

22

Launch Kourou

Agenda

Programme status






Questions / answers

30

JUICE Subcontracted Items

31

87 items are subcontracted in the frame of

JUICE development

• 4 contractors selected as part of Core Team,

o CSW development support

o Structural analysis support

o Operations & database support

o Mission simulator

• 2 contractors pre-selected by Airbus, then

endorsed by ESA,

o Spacecraft Interface Simulator,

o Structure Central Cylinder

• 4 contractors expected to be pre-selected by

subsystem contractors for ESA/Airbus

endorsement

o PCDU

o CDMU

o Solar panel Substrates

o Photo-Voltaic Assembly

o Main Engine

• 2 contractors already kicked-off by ESA, to be

subsumed in prime contract

o CPPA

o Radiation Monitor

JUICE Space

Segment

87 Items

Structure, Shielding &

Thermal Subsystem

6 Items (incl. SS Lead)

MAG Boom

Chemical Propulsion

Subsystem


Other Platform Equipment

5 Item

Solar Generator

Subsystem


(ITT in Prime proposal)

Electrical Power

Subsystem


(ITT in Prime proposal)

Communications

Subsystem


Command & Data

Management Subsystem


Sensors and Actuators

6 Items

Battery

Deep Space Transponder

TWTA Ka-band

RFDA

Propellant Tanks

(pre-selected)

Pressurant Tanks

10 N RCT

20 N RCT

Pressure Regulators

TWTA X-band

RIME Antenna

Pressure Transducers

Filters

Latch Valves

Pyro Valves

Fill & Drain Valves

Non-Return Valves

RIU

Central Cylinder

(pre-selected)

Main Engine

Project Office

8 Items

MAIT

4 Items

GSE

18 Items

Central Software

3 Items

CFRP Parts

Metallic Parts

MLI & SLI

Heat Pipes

S.A. Substrates

(procurement acceleration)

Photo-Voltaic Assembly

(procurement acceleration)

Mechanisms

Management & Project Administration

Product Assurance & Safety

Engineering

Parts Procurement

(ESA, subsumed by Prime)

1 Item

Platform

46 Items

Conf. & Doc. Control Support

Schedule control support

EM AIT

RF Suitcase

Spacecraft Interface Simulator

(pre-selected)

CSW development support

(selected for Core Team)

SW Unit Coding & testing

Solar Array Drive

Assembly

MGSE Products

EGSE Products

Medium Gain Antenna

Major Assembly

Reaction Wheels

Inertial Measurement Unit

Sun Acquisition Sensors

Star Trackers

Navigation Cameras

High Gain Antenna

Low Gain Antenna

Structural Analyses Support

(Selected for Core Team) Harness

Operations & Database Support

(Selected for Core Team)

Q.A. Support

RAMS Support

Real-Time Simulator

Spacecraft Simulators

Accompanying

Measures

1 Items

Qualification Models Parallel

Development

RIME Ant. QM Parallel Devt

JMU

Spacecraft EM Structure

PFM AIT Support Tasks

On-Ground Purging System

Antennas

3 Items

Instrument Supporting

Equipment

3 Items

RADEM

(ESA, subsumed by Prime)

1 Item

Spacecraft Mechancial &

Thermal Test Facilities

Spacecraft Magnetic Test

Facilities

J-MAG Alignment

Calibration System

JMC

AOCS Engineering Support

ISVV

WRTF

Planetary Protection

Engineering Support

PCDU

(Procurement acceleration)

CDMU

(Procurement acceleration)

Flyable Purging Network

RWDI

Mission Simulator Support

(Selected for Core Team)

“Time is of the essence”, ESA and Airbus have already started

the Industrial Consortium build-up

Procurement Approach : 3-step as per ESA requirements

32

ESA

Airbus Defence and Space SAS (FR)JUICE Spacecraft Prime Contractor

· Project Office· Central Software

· Spacecraft EM AIT

· Electrical system engineering· Instruments management support· Spacecraft PFM AIT

Airbus DS GmbH (DE)

NMS Core Team Partners:· Operations & Database support:

CS Romania (RO)· Structural Analyses support: Serenum (CZ)· Central Software development support:

Mobica (PL)

Structure, Shielding, Thermal

subsystem(SSTS)

SSTS equipment& services

Other Spacecraft Equipment &

Services

Chemical Propulsion subsystem

(CPS)

Solar Generator subsystem

(SGS)

Electrical Power subsystem

(EPS)

Command & Data Management

subsystem(CDMS)


(COMS)

CPS equipment& services

SGS equipment & services

EPS equipment& services

CDMS equipment& services

COMS equipment& services

Central CylinderCASA Espacio (ES)

Propellant Tanks

TBD (tbd)

Spacecraft Interface Simulator

(SIS)SSBV Rovsing (DK)

Subsystems

CPPAAlter (ES)

Mission Analysis SupportAirbus DS Ltd (UK)

Equipment & Services

RADEMEfacec

(PT)

Core Team

Mission Simulator: Vectronic (DE)

1st P

rocu

remen

t Step2

nd

Pro

curem

ent Step

3rd

Pro

curem

ent Step

Step 1 : Core Team

Step 2 : Subsystems and

directly procured items

Step 3 : Subsystem items

Industrial Consortium Build-Up Schedule Logic

33

AIV PlanDevelopment

ScheduleSchedule Margin

Policy

Required ItemDelivery Date

RFI Market Survey

Estimated ItemLead Time

Need Date forItem Kick-Off

Selection Procedure

Recommendation for Selection at JPB Meeting #i

Industrial Procurement Plan

Schedule

· List of selected items per JPB meeting· Date of selection of each item· Date for item ITT release

Estimated Subsystem Preliminary Design Time

Need Date forSubsystem Kick-Off

The industrial Consortium build-up logic

is managed through the Industrial

Procurement Plan, and is driven by

The Spacecraft AIT EM and (P)FM need

dates, as elaborated through the AIV Plan,

The development schedule with

assessment of the equipment lead times,

The system schedule policy, depending on

equipment and system criticalities.

This gives equipment kick-off dates.

Considering the schedule constrains

coming from ESA Best Practices

application

The IPP schedule is consolidated,

The equipment ITT issue dates are frozen.

87 items have to be allocated in European industry, at an average rate of 3 items per month To allocate most of the subcontracts at S/C PDR (March 2017),

Each ITT process will take about 6 months from ITT preparation up to subcontractor negotiation and kick-off,

In the core of the procurement activities, about 18 ITT process will run in parallel with different maturity stages,

JUICE procurement effort is already started, key to meet project challenges ITT documents (e.g. specification and SOW) maturity is a must,

Milestones shall be achieved at planned dates, which will be frozen on a quarterly/monthly basis.

Industrial Consortium Build-Up

Sequence

34

The industrial Consortium build-up sequence is

adapted to JUICE challenges

Addressing partly the German SME and New Member States

geo-return in Core Team at start,

Pre-selecting schedule critical equipment (SIS, Central Cylinder,

Propellant Tank) during Prime proposal phase,

RADEM and CPPA started in advance by ESA, to be then

subsumed in prime contract,

3-step approach implemented (introduction of 6 subsystems),

ITT package for urgent items (SGS, EPS, CDMS) posted on

EMITS in June ‘15 before Prime contract awarding by ESA,

Subsystem bidders are authorised to pre-select schedule-critical

equipment.

As authorised by ESA through tailoring of ESA

science procurement policy

JUICE Spacecraft Prime ContractorAirbus Defence and Space SAS (FR)

System Support and AIT Airbus DS GmbH (DE)

Mission Analysis SupportAirbus Defence and Space Ltd (UK)

Preselected Schedule-critical Equipment· Structure Central Cylinder : CASA Espacio (ES)· Propulsion Propellant Tanks : MAN Technologies Aerospace (DE)· Spacecraft Interface Simulator : SSBV Rovsing (DK)

Core Team Size < 35%

Procurement Acceleration

ESA

Spacecraft Prime ContractorAirbus Defence and Space SAS

Airbus DS GmbH

Subsystems Lead contractors

To be selected (Best Practices)

Subsystems Equipment and

Services To be selected (Best Practices)

Project Office Support Tasks To be selected (Best Practices)

Other platform Equipment

To be selected (Best Practices)

Spacecraft AIT support tasks, GSE

and FacilitiesTo be selected (Best Practices)

Confirmation of Pre-Selected Equipment Suppliers

Selection of schedule-critical subsystems (EPS, CDMS, SGS) and Equipment (WRTF, PCDU, CDMU)

Selection of Urgent Platform Equipment

Selection of Remaining Subsystems Suppliers

Selection of Remaining Platform Equipment

Suppliers

Selection of Remaining Subsystem Equipment

Suppliers

Selection of GSE and Test Facilities Suppliers

Selection of Remaining Core Team Support Tasks

Providers

ESA Requirements

CPPA and RADEM Suppliers Selected by ESA

Subsystem Layer

Code of Best Practices

Procurement Acceleration

Geo-Return Requirements

Industrial Responsibility Outside Big-4 & LSI

SME Return

NMS Partners in Core Team

Selection of Additional QM Development Supplier in

NMS

Implementation of Accompanying Measures for

NMS

Special Measures for NMS (CZ, PL, RO)

Airbus support to NMS Suppliers

Vectronic

Core Team Partners in NMS CS Ro / SERENUM / Mobica

Phase B2 K.O.

Phase B2 SRR

PDR

Mission SimulatorVectronic (DE)

Core Team Operations & DB Mechan. Engin. CSW DevelopmentNMS Partners CS Romania (RO) SERENUM (CZ) MOBICA (PL)

Subsumed contracts:CPPA: Alter (ES)

RADEM: EFACEC (PT)

Airbus DS Ltd

JUICE Procurement Industrial Policy Considerations

JUICE procurement is run according to ESA Best Practices in the

frame of a “Large” science mission

All ESA member States are contributing and expecting a fair return

Focus put by Member States and IPC on fair return :

Outside of Big-4 countries (DE, FR, IT, UK) and of Large System Integrators

(Airbus DE/FR/UK, TAS FR/IT, OHB DE),

In New Member States (CZ, PL, RO, for 5.5%),

For German SMEs (10% of the overall achieved DE return),

Not forgetting Member States with critical geo-return situation

JUICE procurement effort is already started, key to meet project

challenges

The initial geographical distribution status includes the allocated work of the core

team for Spacecraft Prime and AIT;

Complemented by a limited set of Core Team support activities in New Member States and

German SME

The geo return situation is continuously monitored by ESA and the prime;

In the Best Practices selection procedure, the recommendation by the Joint

Procurement Board takes into account the geographical return assessment (actual

vs requirement), reported to the Senior Procurement Board as part of the decision-

making material.

35

Member State

Return Requirements

%

Austria 2.8

Belgium 3.2

Czech Republic 1.2

Denmark 2.3

Finland 1.7

Greece 1.9

Ireland 1.3

Luxembourg 0.2

Netherlands 4.6

Norway 3.6

Poland 3.2

Portugal 1.5

Romania 1.1

Spain 7.9

Sweden 3.6

Switzerland 4.9

Sub-total 45.0

France

55.0 Germany

Italy

United Kingdom

Sub-total 55.0

Total 100.0

Within the 55% for Germany, France, Italy, and the United

Kingdom the following additional requirements shall be respected:

• A minimum return to Germany and France of above 13%

each.

• Maximum return for Italy of 5%.

• No limit for the United Kingdom other than the overall 55%.

Subcontractors selection procedure: ESA Best

Practices ESA/IPC(2012)65 rev.2 and Appendix 1

Amended for JUICE, with for each procurement

item :

there will be a nominated Tender Evaluation Board

(TEB) with participation of ESA, Prime and the Issuing

Company (if different)

TEB recommendation is then reviewed by the Joint

Procurement Board (JPB)

For all competitive tenders, a Senior Procurement

Board (SPB) is making the final decision

Negotiation and kick-off then follows SPB decision

The process for ITT package preparation and

evaluation of offers is made of several steps.

Each ITT will be announced and published on

EMITS.EE

Best Practices Procedure

~3 months between ITT

release and selection

~4 months between ITT

release and kick-off

Preparation of

ITT packages

ITT

packages

cover letter

statement of work

specification

draft subcontract

conditions of tender

evaluation criteria

closing date for receipt of offers

decision on award

of a contract

Receipt,

opening of bids

Tender Opening Board

(TOB)

release

to subcontractors

under

OK ? yes

update of ITT

packagesno

OK ?

Preliminary

assessment(by TEB members)

yes

ESAno

JPB recommendation

TEB report

TEB report

Contractor’s

recommendation

EMITS

Distribution of

admitted

tenders

if OK

if NOK

decision on admissibility,

or re-issue of ITT

Findings,

marking, and

assessment(by TEB members)

Tender Evaluation Board

(TEB)

OK ? yes

Elimination of

uncomplete tenders

no

Drawing-up of

evaluation

report(by TEB members)


(TEB)


(TEB)


(TEB)

Joint Procurement Board

(JPB)

Senior Procurement Board

(SPB)


(TEB)

Overall

assessment

step 1

step 2

step 3

step 4

TOB report

36

JUICE Procurement Schedule - Flight Products (1/3)

The spacecraft procurement items

comprise:

• Platform equipment and software

• Ground Support Equipment and Test

Facilities

• System Support Equipment

• Prime support tasks

For each item, the procurement

plan provides planned dates for

ITT release and kick-off

Platform equipment (and software)

will generally be kicked-off during

the phase B2 or C/D timeframe

• depending on the anticipated design

& development effort and schedule

needs

37

Type

(OC/RC/DN)

ITT package

Release

on EMITS

TEB Kick off

Subsystem

C11 - Structure Shielding and Thermal Subsystem OC 20/10/15 04/01/16 12/02/16

C12 - Chemical Propulsion Subsystem OCDone

30/09/201511/12/15 12/02/16

C13 - Solar Generator Subsystem OCDone

10/06/201518/11/15 12/01/16

C14 - Electrical Power Subsystem OCDone

10/06/201513/11/15 15/01/16

C15 - Central Data Management Subsystem OCDone

10/06/201516/10/15 04/12/15

C16 - Communication Subsystem OC 30/10/15 21/01/16 15/03/16

C17 - Other Platform Equipment

C172 - Harness OC 01/10/16 13/12/16 30/01/17

C18 - Sensors and Actuators

C181 - Inertial Measurement Unit OC 30/03/16 11/06/16 29/07/16

C182 - Sun Acquisition Sensor OC 01/12/16 12/02/17 01/04/17

C183 - Star Tracker OC 30/03/16 11/06/16 29/07/16

C184 - Navigation Camera OC 29/10/15 19/01/16 15/03/16

C185 - Reaction Wheel OC 01/08/16 13/10/16 30/11/16

C186 - Solar Array Drive Assembly DN 30/10/15 na 18/02/16

C19 - Antennas

C191 - Low Gain Antenna OC 01/02/17 15/04/17 02/06/17

C192 - Medium Gain Antenna OC 28/10/15 22/01/16 17/03/16

C193 - High Gain Antenna OC 26/11/15 10/02/16 07/04/16

C1I - Instrument Supporting Equipment

C1I1 - MAG Boom OCDone

02/10/201510/12/15 12/02/16

C1I2 - RIME Antenna OC 27/11/15 12/02/16 14/04/16

C1I3 - J-MAG Alignment Calibration System OC 01/12/16 12/02/17 01/04/17

C1M - Monitoring Equipment

C1M1 - RADEM

C1M3 - JUICE Monitoring Camera (JMC) OC 01/06/16 13/08/16 30/09/16

C1M4 - JUICE Monitoring Unit (JMU) OC 01/10/16 13/12/16 30/01/17

C2 - Accompanying Measures

C21 - RIME Ant. QM Parallel Devt OC 01/01/16 15/02/16 10/04/16

C-2C - Parts Procurement

2CP - CPPA


38

Year

Month

ao

ût-

15

se

pt.

-15

oc

t.-1

5

no

v.-

15

dé

c.-

15

jan

v.-

16

fév

r.-1

6

ma

rs-1

6

av

r.-1

6

ma

i-1

6

juin

-16

juil.-

16

ao

ût-

16

se

pt.

-16

oc

t.-1

6

no

v.-

16

dé

c.-

16

jan

v.-

17

fév

r.-1

7

ma

rs-1

7

av

r.-1

7

ma

i-1

7

juin

-17

juil.-

17

ao

ût-

17

se

pt.

-17

oc

t.-1

7

no

v.-

17

dé

c.-

17

jan

v.-

18

C1x - Subsystems ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C11 - Structure Shielding and Thermal

Subsystem° ° ITT ° ° TEB

Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C12 - Chemical Propulsion Subsystem ° ° ° ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C13 - Solar Generator Subsystem ° ° ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C14 - Electrical Power Subsystem ° ° ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C15 - Central Data Management Subsystem ° ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C16 - Communication Subsystem ° ° ITT ° ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C17 - Other Platform Equipment ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C172 - Harness ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° °

C18 - Sensors and Actuators ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C181 - Inertial Measurement Unit ° ° ° ° ° ° ° ITT ° ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C182 - Sun Acquisition Sensor ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° ° ° °

C183 - Star Tracker ° ° ° ° ° ° ° ITT ° ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C184 - Navigation Camera ° ° ITT ° ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C185 - Reaction Wheel ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° ° ° °

C186 - Solar Array Drive Assembly ° ° ITT ° ° °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

JUICE INDUSTRIAL & PROCUREMENT - Monthly Schedule2015 2016 2017


39

Year

Month

ao

ût-

15

se

pt.

-15

oc

t.-1

5

no

v.-

15

dé

c.-

15

jan

v.-

16

fév

r.-1

6

ma

rs-1

6

av

r.-1

6

ma

i-1

6

juin

-16

juil.-

16

ao

ût-

16

se

pt.

-16

oc

t.-1

6

no

v.-

16

dé

c.-

16

jan

v.-

17

fév

r.-1

7

ma

rs-1

7

av

r.-1

7

ma

i-1

7

juin

-17

juil.-

17

ao

ût-

17

se

pt.

-17

oc

t.-1

7

no

v.-

17

dé

c.-

17

jan

v.-

18

C19 - Antennas ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C191 - Low Gain Antenna ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° °

C192 - Medium Gain Antenna Main Assembly ° ° ITT ° ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C193 - High Gain Antenna ° ° ° ITT ° ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C1I - Instrument Supporting Equipment ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C1I1 - MAG Boom ° ° ° ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C1I2 - RIME Antenna ° ° ° ITT ° ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C1I3 - J-MAG Alignment Calibration System ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° ° ° °

C1M - Monitoring Equipment ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C1M1 - RADEM ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C1M3 - JUICE Monitoring Camera (JMC) ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C1M4 - JUICE Monitoring Unit (JMU) ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° °

C2 - Accompanying Measures ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C21 - RIME Ant. QM Parallel Devt ° ° ° ° ° ITT TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

C-2C - Parts Procurement ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2CP - CPPA ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °


JUICE Procurement Schedule - GSE, Facilities and Support

40

Type

(OC/RC/DN)

ITT package

Release

on EMITS

TEB Kick off

2KA - Spacecraft EGSE

2KA1 - CCS OC 30/03/16 11/06/16 29/07/16

2KA2 - TM/TC SCOE OC 01/12/16 12/02/17 01/04/17

2KA3 - Power SCOE OC 01/11/16 13/01/17 02/03/17

2KA4 - RF SCOE OC 01/10/16 13/12/16 30/01/17

2KA5 - Simulator Front-End OC 01/07/16 12/09/16 30/10/16

2KA6 - PCDU Simulator OC 01/10/16 13/12/16 30/01/17

2KB - Spacecraft MGSE

2KB1 - Containers OC 01/01/17 15/03/17 02/05/17

2KB2 - Stands & Trolleys OC 01/01/17 15/03/17 02/05/17

2KB3 - Lifting & Handling OC 01/02/17 15/04/17 02/06/17

2KB4 - Covers & Protection OC 01/02/17 15/04/17 02/06/17

2KB5 - Offload Devices OC 01/03/17 13/05/17 30/06/17

2KB6 - Adaptors OC 01/03/17 13/05/17 30/06/17

2KB7 - Cleanliness & EV Control OC 01/04/17 13/06/17 31/07/17

2KB8 - S/C EM Structure (SEMS) OC 01/09/16 13/11/16 31/12/16

2KBP - Purging System OC 01/02/17 15/04/17 02/06/17

2KE - RF Suitcase

2KE - RF Suitcase OCDone

10/06/2015

Done

15/09/201530/10/15

2KG - WRTF

2KG - WRTF OC 01/01/17 15/03/17 02/05/17

2KS - Spacecraft Simulators

2KS.12 - Real-Time Simulator OC 01/01/16 14/03/16 01/05/16

2BI3 - AIT Support

2BI3 - AIT Support OC 01/10/17 13/12/17 30/01/18

2BS - S/C Test Facilities

2BS1 - S/C Mechanical/Thermal Test Facilities OC 01/05/17 13/07/17 30/08/17

2BS2 - S/C Magnetic Test Facilities OC 01/05/17 13/07/17 30/08/17

System Support Tasks

2ACB - QA OC 01/04/16 13/06/16 31/07/16

2ACC2 - RAMS OC 01/03/16 13/05/16 30/06/16

2AADB/C/D - Documentation, configuration and scheduleOC 01/02/16 14/04/16 01/06/16

2ADQ2 - AOCS support OC 01/02/16 14/04/16 01/06/16

2ADW - Planetary Protection OC 01/03/16 13/05/16 30/06/16

2LV - ISVV OC 01/12/16 12/02/17 01/04/17

2LC - CSW CFDP OC 01/06/16 13/08/16 30/09/16

GSE & Facilities Grouping is foreseen per family of MGSE

ITT release during phase B2 for the GSE

needed early, and in phase C/D for the rest

of them

Test facilities for spacecraft environment

tests split into :

Magnetic test facilities

Other environmental test facilities

System Support Tasks Most of the ITT issued in first half of 2016

JUICE Procurement Schedule - GSE

41

Year

Month

ao

ût-

15

se

pt.

-15

oc

t.-1

5

no

v.-

15

dé

c.-

15

jan

v.-

16

fév

r.-1

6

ma

rs-1

6

av

r.-1

6

ma

i-1

6

juin

-16

juil.-

16

ao

ût-

16

se

pt.

-16

oc

t.-1

6

no

v.-

16

dé

c.-

16

jan

v.-

17

fév

r.-1

7

ma

rs-1

7

av

r.-1

7

ma

i-1

7

juin

-17

juil.-

17

ao

ût-

17

se

pt.

-17

oc

t.-1

7

no

v.-

17

dé

c.-

17

jan

v.-

18

2KA - Spacecraft EGSE ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2KA1 - CCS ° ° ° ° ° ° ° ITT ° ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2KA2 - TM/TC SCOE ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° ° ° °

2KA3 - Power SCOE ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° ° ° ° °

2KA4 - RF SCOE ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° °

2KA5 - Simulator Front-End ° ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2KA6 - PCDU Simulator ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° °

2KB - Spacecraft MGSE ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2KB1 - Containers ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° ° °

2KB2 - Stands & Trolleys ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° ° °

2KB3 - Lifting & Handling ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° °

2KB4 - Covers & Protection ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° °

2KB5 - Offload Devices ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° °

2KB6 - Adaptors ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° °

2KB7 - Cleanliness & EV Control ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° °

2KB8 - S/C EM Structure (SEMS) ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° ° °

2KBP - Purging System ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° °


JUICE Procurement Schedule - Facilities and Support

42

Year

Month

ao

ût-

15

se

pt.

-15

oc

t.-1

5

no

v.-

15

dé

c.-

15

jan

v.-

16

fév

r.-1

6

ma

rs-1

6

av

r.-1

6

ma

i-1

6

juin

-16

juil.-

16

ao

ût-

16

se

pt.

-16

oc

t.-1

6

no

v.-

16

dé

c.-

16

jan

v.-

17

fév

r.-1

7

ma

rs-1

7

av

r.-1

7

ma

i-1

7

juin

-17

juil.-

17

ao

ût-

17

se

pt.

-17

oc

t.-1

7

no

v.-

17

dé

c.-

17

jan

v.-

18

2KG - WRTF ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2KG - WRTF ° °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2KE - RF Suitcase ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2KE - RF Suitcase ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° ° °

2KS - Spacecraft Simulators ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2KS.12 - Real-Time Simulator ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2BS - S/C Test Facilities ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2BS1 - S/C Mechanical/Thermal Test Facilities ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ITT ° TEBKick

off

2BS2 - S/C Magnetic Test Facilities ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

System Support Tasks ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2ACB - QA ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2ACC2 - RAMS ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2AADB/C/D - Documentation, configuration and

schedule° ° ° ° ° ° ° ° ITT ° TEB

Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2ADQ2 - AOCS support ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2ADW - Planetary Protection ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2LV - ISVV ° ° ° ° ° ° ITT ° TEB °Kick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °

2LC - CSW CFDP ° ° ° ° ° ° ° ITT ° TEBKick

off° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °


Agenda

Programme status






Questions / answers

43

Main assumptions of the programme

All the Best Practices subcontractors activities and prices are pertaining to phase B2/C/D,

unless it is specifically requested to bid for a phase E1 activity.

A breakpoint will be introduced in all subcontracts at the end of Spacecraft phase B2: the

subsequent activities will be subject to formal authorization. For ITT issued by end 2015, this

means that there are two time-frames to be considered :

Time-Frame #1 encompassing Phase B2 and C of the subcontract, up to Subcontract CDR;

Time-Frame # 2 encompassing Phase D from CDR up to DRB.

JUICE is a long duration programme: spacecraft launch in 2022, cruise phase of 7 years.

This has several implications like storage on ground, maintainability, spares approach, EEE

parts, etc. which will be reflected in the ITT’s and must be adequately addressed in the tenders

Prices shall be quoted as :

For advance C/D, in FFP

For phase C/D, in FPV 2014 and FFP

44

Class 1 EEE parts quality shall apply for JUICE flight equipment.

There is a Coordinated Parts Procurement Agent (CPPA) under the responsibility of Airbus

Defence and Space for the JUICE programme.

The selection, evaluation, qualification, screening, and procurement of all EEE parts shall be

the responsibility of the Contractor.

The Tenderers shall provide

A preliminary list of parts,

Evaluation of the related cost of the parts listed above.

This cost shall be detailed for each component and shall cover the cost to buy the components.

It shall not include the cost related to activities to be performed by the CPPA (management of the procurement of

the parts, qualification and lot testing).

EEE parts procurement

45

The S/C model delivery is

phased, as follows: Preliminary spacecraft model will be

provided on the 30th of October 2015

to support supplier proposal and initial

equipment analyses

2nd spacecraft model: post spacecraft

SRR board ( April 2016) to be used

for cat C/D equipment PDR and cat

A/B equipment CDR

3rd spacecraft model: post spacecraft

PDR (April 2017) to be used for cat

C/D equipment CDR )

Radiation hardness

46

Shielding optimization has been run by the prime in order to ensure 50 krad on components.

• Radiation vaults are part of the structure design, unit volume specification is therefore stringent

Detailed spacecraft model will be provided in the course of the development including different

materials and massive elements, instead of “6 faces box”.

Magnetic cleanliness

47

Magnetic disturbances on board JUICE constitue a threat on scientific performances

The only way forward to meet the specification consists in moving sensitive sensors away

from the spacecraft body

• A 10.6 m MAG-Boom is therefore implemented on-board JUICE

This needs to be complemented by other precautions measures

• material, internal accommodation and lay out, shielding

• De-perming of equipment before delivery, and specific precautions during transportation and AIT at all

levels

Proposal contents

48

The proposals shall be presented in several volumes, covering typically:

Vol 1 Cover letter

Vol 2 Technical proposal

Part 1 Technical Description

Part 2 Development and AIV

Part 3 Product Assurance (PA) and Safety

Part 4 Options description (if any)

Vol 3 Implementation and Management Proposal

Vol 4 Financial and Contractual Proposal

Vol 5 Exceptions and Non-compliance Proposal (for Baseline and Options, if any)

Vol 6 Subcontractor Proposals (if any) including RFIs

Evaluation criteria

49

The proposals will be evaluated against evaluation criteria which will be specified for each

ITT together with the weighting factors (and will be provided in the ITT).

For the Platform equipment, typical evaluation criteria are:

Background and experience

Understanding of the requirements and discussion of problem areas

Quality and suitability of proposed programme of work

Adequacy and credibility of the industrial implementation

Compliance with administrative tender conditions and acceptance of the contract conditions

The price is evaluated separately in order to make an overall assessment of tenders as per

the Best Practices.

Nb: target prices are provided in the ITT’s.

Procurement – Contact Persons

50

Name Responsibility Email Tel Nr

Manon Bougy Subsystem and Equipment Contracts

Manager

[email protected] +33(0)5 62 19 53 30

Christine Durand Support, GSE and Facilities Contracts

Manager

[email protected] +33(0)5 62 19 57 31

Marion Hugues Subsystem and Equipment Contracts

Manager

[email protected] +33(0)5 62 19 57 31

Christophe Gabilan Spacecraft Industrial Manager [email protected] +33(0)5 62 19 52 18

Daniel Hakansson Spacecraft Procurement Manager [email protected] +49 75 45 8 83 16

Christian Lebranchu Spacecraft Industrial Manager [email protected] +33(0)5 6219 77 30

Alain Tabouelle Spacecraft Procurement Manager [email protected] +33(0)5 6219 99 29








Thank you, we wish you to make good proposals for

the JUICE Best Practices procurement and to join the

programme

51

1

Coordinate Parts Procurement Agent

F. Panin – JUICE PA Manager October 2015

JUICE Industrial Day

CPPA - Background

2

• The procurement of electronic, electrical, and electromechanical (EEE) components is supported by an Agent with the aim of:

• providing components that meet the quality requirements• guaranteeing the qualification status• providing minimum component cost to users, and the program• assuring reliable sources• reducing the number of component types through standardization• identifying critical components (e.g. due to long lead, obsolescence,

alerts) and proposing alternatives • using stocks available from other ESA projects

CPPA - Contractor

3

• Alter, Spain has been selected by ESA through an ITT process.

• Alter will coordinate orders received by users with the objective of harmonising and standardising components, thus minimising cost, and meeting the applicable quality requirements.

• Alter will support also the export control/ ITAR approval process.

• Coordinated procurement will encompass both instrument and spacecraft users. It will cover Engineering Models (EM), Qualification Models (QMs) and Flight Models (FMs)

CPPA - Status

4

• First User Meeting has been held on 24 March 2015 at Alter

• User registration is taking place

• First orders for Engineering Models have been received

• Cut off dates for next orders will be established by Alter based on the user needs (identification of components and need dates)