juice industry day -...
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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).
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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]
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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
M. Baroni | JUICE_Introduction_for_Industry_Day| Slide 1
ESA and Airbus Defence & Space welcome the participants to the JUICE Industry Day
o 232 participants o 173 companies o 22 countries
Introduction
M. Baroni | JUICE_Introduction_for_Industry_Day| Slide 3
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
M. Baroni | JUICE_Introduction_for_Industry_Day| Slide 4
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
M. Baroni | JUICE_Introduction_for_Industry_Day| Slide 5
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
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 3
Scientific Objectives (1/3)
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 4
Scientific Objectives (2/3)
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 5
Scientific Objectives (3/3)
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 6
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
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 7
Trajectory for cruise phase
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 8
Trajectory for cruise phase
Trajectory for cruise phase : animation
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 9
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
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 10
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
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 11
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
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 12
Spacecraft configuration (2/2)
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 13
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)
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 14
Master Schedule
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 15
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.
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 16
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)
G. Sarri| JUICE_programme_status_for_Industry_1| Slide 17
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.
ESA UNCLASSIFIED – For Official Use
Carla Signorini | ESTEC | 15/09/2011 | Slide 3
ECOS - The Rate File
Rate file noticeable features
Escalation tables
Variable rate agreement
Multiple
Overheads and Profit rates
Average sellable
hours/year
ESA UNCLASSIFIED – For Official Use
Carla Signorini | ESTEC | 15/09/2011 | Slide 4
ESA UNCLASSIFIED – For Official Use
ECOS - Building the PT/WBS with Support Functions
Carla Signorini | ESTEC | 15/09/2011 | Slide 5
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
ESA UNCLASSIFIED – For Official Use
Carla Signorini | ESTEC | 15/09/2011 | Slide 6
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
ESA UNCLASSIFIED – For Official Use
Carla Signorini | ESTEC | 15/09/2011 | Slide 7
ESA UNCLASSIFIED – For Official Use
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
Carla Signorini | ESTEC | 15/09/2011 | Slide 8
ESA UNCLASSIFIED – For Official Use
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
Carla Signorini | ESTEC | 15/09/2011 | Slide 9
ESA UNCLASSIFIED – For Official Use
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
Carla Signorini | ESTEC | 15/09/2011 | Slide 10
ESA UNCLASSIFIED – For Official Use
ECOS - A global view over the price
Carla Signorini | ESTEC | 15/09/2011 | Slide 11
ECOS - Advanced features
ESA UNCLASSIFIED – For Official Use
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
Carla Signorini | ESTEC | 15/09/2011 | Slide 12
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
ESA UNCLASSIFIED – For Official Use
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
Mission and spacecraft configuration
Verification logic and development schedule
Procurement approach
Main Tender Conditions
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
Project and industrial organisation
Mission and spacecraft configuration
Verification logic and development schedule
Procurement approach
Main Tender Conditions
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
The JUICE spacecraft (2/3)
11
The JUICE spacecraft (3/3)
12
Functional architecture
13
Solar Generator Subsystem
Payload
Chemical
Propulsion
Subsystem
Command and Data
Management Subsystem
Attitude
and Orbit
Control
Electrical and Power
Subsystem
Communications 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
Project and industrial organisation
Mission and spacecraft configuration
Verification logic and development schedule
Procurement approach
Main Tender Conditions
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
Project and industrial organisation
Mission and spacecraft configuration
Verification logic and development schedule
Procurement approach
Main Tender Conditions
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
13 Items (incl. SS Lead)
Other Platform Equipment
5 Item
Solar Generator
Subsystem
4 Items (incl. SS Lead)
(ITT in Prime proposal)
Electrical Power
Subsystem
3 Items (incl. SS Lead)
(ITT in Prime proposal)
Communications
Subsystem
5 Items (incl. SS Lead)
Command & Data
Management Subsystem
3 Items (incl. SS Lead)
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)
Communications subsystem
(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)
Tender Evaluation Board
(TEB)
Tender Evaluation Board
(TEB)
Tender Evaluation Board
(TEB)
Joint Procurement Board
(JPB)
Senior Procurement Board
(SPB)
Tender Evaluation Board
(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
JUICE Procurement Schedule - Flight Products (2/3)
38
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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
JUICE Procurement Schedule - Flight Products (3/3)
39
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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 INDUSTRIAL & PROCUREMENT - Monthly Schedule2015 2016 2017
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
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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 INDUSTRIAL & PROCUREMENT - Monthly Schedule2015 2016 2017
JUICE Procurement Schedule - Facilities and Support
42
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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° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° ° °
JUICE INDUSTRIAL & PROCUREMENT - Monthly Schedule2015 2016 2017
Agenda
Programme status
Project and industrial organisation
Mission and spacecraft configuration
Verification logic and development schedule
Procurement approach
Main Tender Conditions
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)