We make it flyby. JUICE Industry Day. - Noordwijk, October 27/28th, JUI-ASFT-SYS-HO-024

Transcription

1 We make it flyby JUICE Industry Day - Noordwijk, October 27/28th, JUI-ASFT-SYS-HO-024

2 Agenda Programme status Project Team organisation Industrial organisation Mission and spacecraft configuration Verification logic and development schedule Procurement approach Main Tender Conditions Questions / answers 2

3 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

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, 16 th 2015 ESA / Airbus negotiation successfully completed on July, 24 th with ESA held on July,28 th This is 2 months ahead of the initial plan (ITT) Fixed launch date on May, 20 th 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) Date 4-4

5 Agenda Programme status Project and industrial organisation Mission and spacecraft configuration Verification logic and development schedule Procurement approach Main Tender Conditions Questions / answers 5

6 The Prime Project Team - A fully integrated joint team Project Manager Vincent Poinsignon Satellite Design Authority Philippe Temporelli Instruments Expert Gilles Planche Secretariat and Documentation Lydie Pinel Project Control Maité Aimé FHN Local Project Manager Markus Faust Schedule Control Dominique de Bruyn Contract Officer Christine Durand Subcontracts Manon Bougy / Marion Hugues Product Assurance Manager Pierre Thoral Configuration Manager Damien de Paysac System Engineering Manager Frédéric Faye Development, AIV and TDA Thomas Schirmann Industrial Manager Christian Lebranchu AIT Manager Philippe Durand Instrument Team Manager Xavier Moisson Mission & System performances Cyril Cavel Deputy Christophe Gabilan EM AIT Philippe Durand Industrial Development Expertise Stephane Osipenco Procurement Coordination Alain Tabouelle PFM AIT Thilo Nacke Spacecraft architects Mission analysis Steve Kemble Avionics Philippe Humbert Radiations Thierry Bouchet AOCS & Navigation Pascal Régnier Magnetic/EMC Markus Faust FDIR, Operations & database Eric Ecale CDMS Philippe Humbert Software Luc maillet Mechanical, Thermal & Propulsion Philippe Moinard Functional Verification Frédéric Juillard Mechanical & Structure Sébastien Laborde Thermal Anthony Darel Electrical Helmut Gramatke Mechanisms Charles Lambert Power Clemens Kalde Rime antenna & MAG boom Hans Joachim Schoedel RF Communications Robert Purvinskis Propulsion Philippe Moinard Magnetic performance Klaus Bubeck Solar Generator Didier Loche EMC / RMC cleanliness John Aulton Technical Officers for the in-situ, radio and radar instruments PEP RPWI JMAG 3GM RIME Uwe Kummer Stephane Osipenco Stephane Osipenco Michael Chwalla Uwe Kummer Technical Officers for the optical instruments SWI JANUS MAJIS UVS GALA Jean Marc Goutoule Xavier Moisson Benjamin Massart Benjamin Massart Michael Chwalla 6

7 JUICE Industrial Organisation ESA Electrical system engineering Instruments management support Spacecraft PFM AIT Airbus DS GmbH (DE) Mission Analysis Support Airbus DS Ltd (UK) Airbus Defence and Space SAS (FR) JUICE Spacecraft Prime Contractor Project Office AOCS and Central Software Spacecraft EM AIT Mission Simulator: Vectronic (DE) NMS Core Team Partners: Operations & Database support: CS Romania (RO) Structural Analyses support: Serenum (CZ) Central Software development support: Mobica (PL) Core Team Layer Structure, Shielding, Thermal subsystem (SSTS) Chemical Propulsion subsystem (CPS) Solar Generator subsystem (SGS) Electrical Power subsystem (EPS) Command & Data Management subsystem (CDMS) Communications subsystem (COMS) Subsystem Layer SSTS equipment & services CPS equipment & services SGS equipment & services EPS equipment & services CDMS equipment & services COMS equipment & services Central Cylinder CASA Espacio (ES) Core Team Best Practices ESA selected contractors Propellant Tanks To be selected Pre-selected critical equipment CPPA: Alter (ES) RADEM: Efacec (PT) Spacecraft Interface Simulator (SIS) SSBV Rovsing (DK) Other Spacecraft Equipment & Services Equipment and Services Layer 7

8 Agenda Programme status Project and industrial organisation Mission and spacecraft configuration Verification logic and development schedule Procurement approach Main Tender Conditions Questions / answers 8

9 JUICE key figures 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 9

10 The JUICE spacecraft (1/3) 10

11 The JUICE spacecraft (2/3) 11

12 The JUICE spacecraft (3/3) 12

13 Functional architecture. 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 Payload 3GM JANUS SWI GALA UVS J-MAG MAJIS RIME RPWI RADEM PEP SpaceWire Chemical Propulsion Subsystem Main Engine Reaction Control Thrusters Command and Data Management Subsystem Remote Interface Unit Command and Data Management Unit Datation pulse Reaction Reaction Wheel Wheel Reaction Reaction Wheel Wheel Star Star Tracker Tracker Electronics Electronics Inertial Measurement Unit (including accelerometers) Star Tracker Star Star Tracker Optical Tracker Head Optical Optical Head Head Attitude and Orbit Control MIL-STD-1553 B data bus Antenna Pointing Mechanism Electronics Travelling X-bandWave Travelling Tube Amplifiers Wave (X-band, Tube Amplifier Ka-band) Deep Deep Space Space Transponder Deployment lines Protected power lines Thermal control Sun Sun Sensor Sensor Navigation Camera Antenna Pointing Mechanism RF Distribution Assembly Travelling Ka-band Wave Travelling Tube Amplifiers Wave (X-band, Tube Amplifier Ka-band) Power Control and Distribution Unit Solar Array Drive Electronics JUICE Monitoring Unit JUICE Monitoring Camera Communications subsystem Battery Solar Array Drive Mechanism Solar Array Medium Gain Antenna Low Gain Antenna High Gain Antenna Electrical and Power Subsystem Solar Generator Subsystem 13

14 Electrical architecture. 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 14

15 Electrical Power Subsystem 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. 15

16 Communication Subsystem and Antennas 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). 16

17 Control & Data Management Subsystem 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 crossstrapping 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. 17

18 Thermal Control Concept 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. 18

19 AOCS Functional Chain 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 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. 19

20 EMC requirements Vaults and Harness are designed to ensure a maximum EMC tightness External surfaces, including solar cells, are conductive 20

21 Magnetic cleanliness requirements 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 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

22 Robustness to radiations (1/2) 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 o total dose of 2 Grad outside spacecraft, 1 Mrad inside the vaults and 50 krad inside electronics of vaults External harness has to withstand typically 10 Mrad. 22

23 Robustness to radiations (2/2) 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. 23

24 Agenda Programme status Project and industrial organisation Mission and spacecraft configuration Verification logic and development schedule Procurement approach Main Tender Conditions Questions / answers 24

25 Development Drivers Launch on June, 1 st 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

26 Development Logic, Phases and Reviews PHASE B2 : Preliminary Definition Phase PHASE C/D : Detailed Definition, Production and Verification Phase PHASE E1: Launch and Commissioning Phase -Off SRR PDR CDR FAR NECR Spacecraft Level System Requirements Consolidation Preliminary Design Development Plan Consolidation Detailed Design and Performances Consolidation (Budgets and Analysis / Review of Design) Performances Validation and Consolidation Early Functional, EMC and Magnetic Verification on Spacecraft EM Early Thermal Verification on TDM In-flight Performance Verification Instrument Interface Consolidation Late Interface Modification Spacecraft PFM Integration and Qualification Launch Campaign Spacecraft Commissioning IPDR ICDR IFDR Instrument Level Instruments Preliminary Design Instruments Detailed Design Instruments Manufacturing & Qualification Provision for Instruments Staggered Delivery Subsystem & Equipment ITT Preparation Subsystem & Equipment Level Subsystem & Equipment Selection Process S/S -Off Subsystem Preliminary Design Eqpt -Off S/S PDR Eqpt PDR Subsystem Detailed Design Eqpt CDR S/S CDR Subsystem Qualification Eqpt QR S/S QR Equipment design Equipment Development & Qualification Flight Model Acceptance Technology Development ESA Technology Development Activities Additional Technology Development Activities 26

27 This image cannot currently be displayed. This image cannot currently be displayed. Model Philosophy (AOCS) FAME Real Time Simulator SVF CCS CDMU EBB RF Suitcase AOCS Performance Verification Software Verification Subset of Func. Verif. Test Procedure TRSP EM Ground Segment RFCT Equip./Instrument EM S/C EM Heritage & Technology Development Activities Eqpt./Instr. Development Equip./ Instrument EQM Complete Func. Verif. Conducted EMC AC Magnetic charac. SVT with MOC Eqpt / Instrument PFM Early Functional, EMC and Magnetic Verification S/C PFM Key Hardware Flow Eqpt./Inst.Qualification Equip./Instrument Acceptance or Delta- Qualification Structure PFM Early Mechanical Verification Build acceptance Mechanical & Thermal Qualification EMC Qualification SVT with MOC Development Logic Flow System Level Static tests Early Thermal Verification S/S or Equipment Level S/C TDM Thermal test 27

28 Verification Levels within Industrial Chain COMS CDMS EPS TRSP Qual. And Accept. TWTA Qual. And Accept. RFDA Qual. And Accept. CDMU Qual. And Accept. RIU Qual. And Accept. Battery Qual. And Accept. PCDU Qual. And Accept. COMS Subsystem Qual. And Acceptance CDMS Subsystem Qual. And Acceptance EPS Subsystem Qual. And Acceptance Prime Contractor Technology Development Activities Scientific Instruments Central Software Development ESA TDA s Industry TDA s Instrument Qual. And Acceptance Early Instrument Interface Verification with SIS EMs FMs Early Functional, EMC and Magnetic Verification on S/C EM Platform Equipment Secondary Structure S/C PFM Integration Key FM Flow EM Flow System Level Subsystem level Equipment level Instrument level Sensors & Actuators Qual. And Acceptance Antennas Qual. And Acceptance Instruments Support HW Qual. And Acceptance RADEM Qual. And Acceptance Other Platform Equipment Qual. And Acceptance SSTS MLI Qual. And Acceptance Structure Qual. And Acceptance Early Thermal Verification on TDM Primary Structure CPS CPS Components Qual. And Acceptance CPS Assembly on S/C Structure CPS Subsystem Qual. And Acceptance Assembled Structure/CPS SGS SGS Qualification and Acceptance S/C PFM Qualification and Acceptance 28

29 Transportation Plan Road transport from Friedrichshafen to ESTEC Noordwijk (for environmental test) ETS Noordwijk 2 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) 5 Launch Kourou AIRBUS DS Friedrichshafen 1 3 IABG Ottobrunn Flight transport from Toulouse to Kourou (launch campaign) AIRBUS DS Toulouse 4 29

30 Agenda Programme status Project and industrial organisation Mission and spacecraft configuration Verification logic and development schedule Procurement approach Main Tender Conditions Questions / answers 30

31 JUICE Subcontracted Items JUICE Space Segment 87 Items Project Office 8 Items Central Software 3 Items Platform 46 Items 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- by ESA, to be subsumed in prime contract o CPPA o Radiation Monitor Management & Project Administration Product Assurance & Safety MAIT 4 Items Engineering Parts Procurement (ESA, subsumed by Prime) 1 Item Conf. & Doc. Control Support Schedule control support EM AIT Q.A. Support RAMS Support Structural Analyses Support (Selected for Core Team) Operations & Database Support (Selected for Core Team) Mission Simulator Support (Selected for Core Team) AOCS Engineering Support Planetary Protection Engineering Support Spacecraft EM Structure PFM AIT Support Tasks Spacecraft Mechancial & Thermal Test Facilities Spacecraft Magnetic Test Facilities CSW development support (selected for Core Team) SW Unit Coding & testing ISVV Accompanying Measures 1 Items Qualification Models Parallel Development RIME Ant. QM Parallel Devt GSE 18 Items EGSE Products MGSE Products WRTF On-Ground Purging System RF Suitcase Spacecraft Simulators Real-Time Simulator Spacecraft Interface Simulator (pre-selected) Structure, Shielding & Thermal Subsystem 6 Items (incl. SS Lead) Central Cylinder (pre-selected) CFRP Parts Metallic Parts MLI & SLI Heat Pipes Chemical Propulsion Subsystem 13 Items (incl. SS Lead) Propellant Tanks (pre-selected) Pressurant Tanks Main Engine 10 N RCT 20 N RCT Pressure Regulators Pressure Transducers Filters Latch Valves Pyro Valves Fill & Drain Valves Non-Return Valves Solar Generator Subsystem 4 Items (incl. SS Lead) (ITT in Prime proposal) S.A. Substrates (procurement acceleration) Photo-Voltaic Assembly (procurement acceleration) Mechanisms Electrical Power Subsystem 3 Items (incl. SS Lead) (ITT in Prime proposal) Communications Subsystem 5 Items (incl. SS Lead) Deep Space Transponder TWTA X-band TWTA Ka-band RFDA Other Platform Equipment 5 Item Flyable Purging Network Harness JMU JMC RWDI Sensors and Actuators 6 Items Inertial Measurement Unit Sun Acquisition Sensors Star Trackers Navigation Cameras Reaction Wheels Solar Array Drive Assembly Antennas 3 Items Low Gain Antenna Medium Gain Antenna Major Assembly High Gain Antenna Instrument Supporting Equipment 3 Items PCDU (Procurement acceleration) MAG Boom Time is of the essence, ESA and Airbus have already started the Industrial Consortium build-up 31 Battery Command & Data Management Subsystem 3 Items (incl. SS Lead) CDMU (Procurement acceleration) RIU RIME Antenna J-MAG Alignment Calibration System RADEM (ESA, subsumed by Prime) 1 Item

32 Procurement Approach : 3-step as per ESA requirements Step 1 : Core Team Step 2 : Subsystems and directly procured items Step 3 : Subsystem items Electrical system engineering Instruments management support Spacecraft PFM AIT Airbus DS GmbH (DE) Structure, Shielding, Thermal subsystem (SSTS) SSTS equipment & services Central Cylinder CASA Espacio (ES) Chemical Propulsion subsystem (CPS) CPS equipment & services Propellant Tanks TBD (tbd) Solar Generator subsystem (SGS) SGS equipment & services Mission Analysis Support Airbus DS Ltd (UK) Electrical Power subsystem (EPS) EPS equipment & services ESA Airbus Defence and Space SAS (FR) JUICE Spacecraft Prime Contractor Project Office Central Software Spacecraft EM AIT Command & Data Management subsystem (CDMS) CDMS equipment & services Mission Simulator: Vectronic (DE) Communications subsystem (COMS) COMS equipment & services Core Team Subsystems Equipment & Services NMS Core Team Partners: Operations & Database support: CS Romania (RO) Structural Analyses support: Serenum (CZ) Central Software development support: Mobica (PL) Other Spacecraft Equipment & Services CPPA Alter (ES) RADEM Efacec (PT) Spacecraft Interface Simulator (SIS) SSBV Rovsing (DK) 1st Procurement Step 2nd Procurement Step 3rd Procurement Step 32

33 Industrial Consortium Build-Up Schedule Logic 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. AIV Plan Selection Procedure Development Schedule Required Item Delivery Date Schedule Margin Policy Need Date for Item -Off Estimated Item Lead Time RFI Market Survey Estimated Subsystem Preliminary Design Time This gives equipment kick- dates. Considering the schedule constrains coming from ESA Best Practices application The IPP schedule is consolidated, The equipment ITT issue dates are frozen. Recommendation for Selection at JPB Meeting #i Need Date for Subsystem -Off Industrial Procurement Plan Schedule List of selected items per JPB meeting Date of selection of each item Date for item ITT release 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-, 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. 33

34 Industrial Consortium Build-Up Sequence The industrial Consortium build-up sequence is adapted to JUICE challenges System Support and AIT Airbus DS GmbH (DE) CPPA and RADEM Suppliers Selected by ESA JUICE Spacecraft Prime Contractor Airbus Defence and Space SAS (FR) Mission Analysis Support Airbus Defence and Space Ltd (UK) Mission Simulator Vectronic (DE) Core Team Operations & DB Mechan. Engin. CSW Development NMS Partners CS Romania (RO) SERENUM (CZ) MOBICA (PL) Preselected Schedule-critical Equipment Structure Central Cylinder : CASA Espacio (ES) Propulsion Propellant Tanks : MAN Technologies Aerospace (DE) Spacecraft Interface Simulator : SSBV Rovsing (DK) ESA Requirements Core Team Size < 35% SME Return NMS Partners in Core Team Procurement Acceleration Addressing partly the German SME and New Member States geo-return in Core Team at start, Phase B2 K.O. ESA Pre-selecting schedule critical equipment (SIS, Central Cylinder, Propellant Tank) during Prime proposal phase, Airbus DS GmbH Spacecraft Prime Contractor Airbus Defence and Space SAS Vectronic RADEM and CPPA started in advance by ESA, to be then subsumed in prime contract, Airbus DS Ltd Subsumed contracts: CPPA: Alter (ES) RADEM: EFACEC (PT) Subsystems Lead contractors To be selected (Best Practices) Core Team Partners in NMS CS Ro / SERENUM / Mobica Subsystem Layer 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. Phase B2 SRR Spacecraft AIT support tasks, GSE and Facilities To be selected (Best Practices) Confirmation of Pre-Selected Equipment Suppliers Subsystems Equipment and Services To be selected (Best Practices) Other platform Equipment To be selected (Best Practices) Project Office Support Tasks To be selected (Best Practices) Selection of schedule-critical subsystems (EPS, CDMS, SGS) and Equipment (WRTF, PCDU, CDMU) Code of Best Practices Procurement Acceleration As authorised by ESA through tailoring of ESA science procurement policy Selection of Remaining Core Team Support Tasks Providers Selection of Urgent Platform Equipment Selection of Remaining Subsystems Suppliers Industrial Responsibility Outside Big-4 & LSI Selection of GSE and Test Facilities Suppliers Selection of Remaining Platform Equipment Suppliers Selection of Remaining Subsystem Equipment Suppliers Geo-Return Requirements 34 PDR Implementation of Accompanying Measures for NMS Selection of Additional QM Development Supplier in NMS Airbus support to NMS Suppliers Special Measures for NMS (CZ, PL, RO)

35 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 decisionmaking 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 Germany 55.0 Italy United Kingdom Sub-total 55.0 Total 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%.

36 Best Practices Procedure update of ITT packages no if NOK 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- then follows SPB decision step 1 step 2 step 3 Preparation of ITT packages Receipt, opening of bids Preliminary assessment (by TEB members) ITT packages Tender Evaluation Board (TEB) cover letter statement of work specification draft subcontract conditions of tender evaluation criteria closing date for receipt of ers Tender Opening Board (TOB) OK? TOB report yes no OK? Findings, marking, and assessment (by TEB members) ESA if OK yes OK? Distribution of admitted tenders yes decision on admissibility, or re-issue of ITT Drawing-up of evaluation report (by TEB members) release to subcontractors under EMITS Tender Evaluation Board (TEB) The process for ITT package preparation and evaluation of ers is made of several steps. Each ITT will be announced and published on EMITS.EE no Tender Evaluation Board (TEB) Elimination of uncomplete tenders Overall assessment Tender Evaluation Board (TEB) Tender Evaluation Board (TEB) TEB report decision on award of a contract step 4 TEB report ~3 months between ITT release and selection ~4 months between ITT release and kick- Contractor s recommendation Joint Procurement Board (JPB) JPB recommendation Senior Procurement Board (SPB) 36

37 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- Platform equipment (and software) will generally be kicked- during the phase B2 or C/D timeframe depending on the anticipated design & development effort and schedule needs Type (OC/RC/DN) ITT package Release on EMITS TEB Subsystem C11 - Structure Shielding and Thermal Subsystem OC 20/10/15 04/01/16 12/02/16 C12 - Chemical Propulsion Subsystem OC Done 30/09/ /12/15 12/02/16 C13 - Solar Generator Subsystem OC Done 10/06/ /11/15 12/01/16 C14 - Electrical Power Subsystem OC Done 10/06/ /11/15 15/01/16 C15 - Central Data Management Subsystem OC Done 10/06/ /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 OC Done 02/10/ /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 37

38 JUICE Procurement Schedule - Flight Products (2/3) Year JUICE INDUSTRIAL & PROCUREMENT - Monthly Schedule Month août-15 sept.-15 oct.-15 nov.-15 déc.-15 janv.-16 févr.-16 mars-16 avr.-16 mai-16 juin-16 juil.-16 août-16 sept.-16 oct.-16 nov.-16 déc.-16 janv.-17 févr.-17 mars-17 avr.-17 mai-17 juin-17 juil.-17 août-17 sept.-17 oct.-17 nov.-17 déc.-17 janv.-18 C1x - Subsystems C11 - Structure Shielding and Thermal Subsystem ITT TEB C12 - Chemical Propulsion Subsystem TEB C13 - Solar Generator Subsystem TEB C14 - Electrical Power Subsystem TEB C15 - Central Data Management Subsystem TEB C16 - Communication Subsystem ITT TEB C17 - Other Platform Equipment C172 - Harness ITT TEB C18 - Sensors and Actuators C181 - Inertial Measurement Unit ITT TEB C182 - Sun Acquisition Sensor ITT TEB C183 - Star Tracker ITT TEB C184 - Navigation Camera ITT TEB C185 - Reaction Wheel ITT TEB C186 - Solar Array Drive Assembly ITT 38

39 JUICE Procurement Schedule - Flight Products (3/3) Year JUICE INDUSTRIAL & PROCUREMENT - Monthly Schedule Month août-15 sept.-15 oct.-15 nov.-15 déc.-15 janv.-16 févr.-16 mars-16 avr.-16 mai-16 juin-16 juil.-16 août-16 sept.-16 oct.-16 nov.-16 déc.-16 janv.-17 févr.-17 mars-17 avr.-17 mai-17 juin-17 juil.-17 août-17 sept.-17 oct.-17 nov.-17 déc.-17 janv.-18 C19 - Antennas C191 - Low Gain Antenna ITT TEB C192 - Medium Gain Antenna Main Assembly ITT TEB C193 - High Gain Antenna ITT TEB C1I - Instrument Supporting Equipment C1I1 - MAG Boom TEB C1I2 - RIME Antenna ITT TEB C1I3 - J-MAG Alignment Calibration System ITT TEB C1M - Monitoring Equipment C1M1 - RADEM C1M3 - JUICE Monitoring Camera (JMC) ITT TEB C1M4 - JUICE Monitoring Unit (JMU) ITT TEB C2 - Accompanying Measures C21 - RIME Ant. QM Parallel Devt ITT TEB C-2C - Parts Procurement 2CP - CPPA 39

40 JUICE Procurement Schedule - GSE, Facilities and Support 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 Type (OC/RC/DN) ITT package Release on EMITS TEB 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 OC Done 10/06/2015 Done 15/09/ /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 sc OC 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 40

41 JUICE Procurement Schedule - GSE Year JUICE INDUSTRIAL & PROCUREMENT - Monthly Schedule Month août-15 sept.-15 oct.-15 nov.-15 déc.-15 janv.-16 févr.-16 mars-16 avr.-16 mai-16 juin-16 juil.-16 août-16 sept.-16 oct.-16 nov.-16 déc.-16 janv.-17 févr.-17 mars-17 avr.-17 mai-17 juin-17 juil.-17 août-17 sept.-17 oct.-17 nov.-17 déc.-17 janv.-18 2KA - Spacecraft EGSE 2KA1 - CCS ITT TEB 2KA2 - TM/TC SCOE ITT TEB 2KA3 - Power SCOE ITT TEB 2KA4 - RF SCOE ITT TEB 2KA5 - Simulator Front-End ITT TEB 2KA6 - PCDU Simulator ITT TEB 2KB - Spacecraft MGSE 2KB1 - Containers ITT TEB 2KB2 - Stands & Trolleys ITT TEB 2KB3 - Lifting & Handling ITT TEB 2KB4 - Covers & Protection ITT TEB 2KB5 - Offload Devices ITT TEB 2KB6 - Adaptors ITT TEB 2KB7 - Cleanliness & EV Control ITT TEB 2KB8 - S/C EM Structure (SEMS) ITT TEB 2KBP - Purging System ITT TEB 41

42 JUICE Procurement Schedule - Facilities and Support Year JUICE INDUSTRIAL & PROCUREMENT - Monthly Schedule Month août-15 sept.-15 oct.-15 nov.-15 déc.-15 janv.-16 févr.-16 mars-16 avr.-16 mai-16 juin-16 juil.-16 août-16 sept.-16 oct.-16 nov.-16 déc.-16 janv.-17 févr.-17 mars-17 avr.-17 mai-17 juin-17 juil.-17 août-17 sept.-17 oct.-17 nov.-17 déc.-17 janv.-18 2KG - WRTF 2KG - WRTF 2KE - RF Suitcase 2KE - RF Suitcase ITT TEB 2KS - Spacecraft Simulators 2KS.12 - Real-Time Simulator ITT TEB 2BS - S/C Test Facilities 2BS1 - S/C Mechanical/Thermal Test Facilities ITT TEB 2BS2 - S/C Magnetic Test Facilities System Support Tasks 2ACB - QA 2ACC2 - RAMS 2AADB/C/D - Documentation, configuration and schedule ITT TEB 2ADQ2 - AOCS support ITT TEB 2ADW - Planetary Protection ITT TEB 2LV - ISVV ITT TEB 2LC - CSW CFDP ITT TEB 42

43 Agenda Programme status Project and industrial organisation Mission and spacecraft configuration Verification logic and development schedule Procurement approach Main Tender Conditions Questions / answers 43

44 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

45 EEE parts procurement 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). 45

46 Radiation hardness 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. 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 ) 46

47 Magnetic cleanliness 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 47

48 Proposal contents 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 48

49 Evaluation criteria 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. 49

50 Procurement Contact Persons Name Responsibility Tel Nr Manon Bougy Christine Durand Marion Hugues Subsystem and Equipment Contracts Manager Support, GSE and Facilities Contracts Manager Subsystem and Equipment Contracts Manager +33(0) (0) (0) Christophe Gabilan Spacecraft Industrial Manager +33(0) Daniel Hakansson Spacecraft Procurement Manager Christian Lebranchu Spacecraft Industrial Manager Christian.lebranchu@airbus.com +33(0) Alain Tabouelle Spacecraft Procurement Manager Alain.tabouelle@airbus.com +33(0)

51 Thank you, we wish you to make good proposals for the JUICE Best Practices procurement and to join the programme 51