ESA Plain Document (Silver)emits.sso.esa.int/.../ESTEC/PLATO_Industry_Days_DBI.docx · Web viewFor...
Transcript of ESA Plain Document (Silver)emits.sso.esa.int/.../ESTEC/PLATO_Industry_Days_DBI.docx · Web viewFor...
PLATO Industry Days (PID)
With the present announcement, the European Space Agency and OHB System AG (Germany) inform the EMITS Users (European Companies and Institutes) about a presentation of the PLATO mission, its procurement plan and related business opportunities. The first PLATO Industry Days (PID) will take place on 19-20 September 2018 at:
European Space Research and Technology Centre
(ESTEC)
Keplerlaan 1
2200 AG Noordwijk
(The Netherlands)
1. The PLATO Mission
The PLAnetary Transits and Oscillations of stars mission (PLATO) is the M3 mission in ESA’s Cosmic Vision 2015-2025 Programme.
PLATO aims at finding and characterising a large number of extrasolar planetary systems, with emphasis on the properties of the terrestrial planets in the habitable zone around bright solar-like stars. PLATO also aims at investigating seismic activity in stars, enabling the precise characterisation of the planets’ host star, including its age. PLATO will provide accurate determinations of the planet radii, stellar irradiation, architecture of planetary systems and evolutionary ages/stages. In combination with ground-based observations, PLATO will provide accurate planetary masses and mean densities.
For achieving its science objectives, PLATO relies on high-precision photometry to produce a science data product consisting of a large sample of stellar light curves and astrometry measurements, obtained over time intervals of months to several years with a high duty cycle.
The scientific payload consists of 26 Cameras with a wide combined field of view of ~2250 deg2, performing photometric observation a visible wavelengths and their the associated digital and analogue electronics. During science observations, the payload will produce a large number of high-accuracy stellar-lightcurves and images over large fields and targets that will be downlinked to ground for further calibration and data-processing in order to produce the required times series for scientific analysis.
PLATO will be launched from the Guiana Space Centre, Kourou, with a medium size launcher vehicle into a transfer to a large orbit around the second Lagrangian Point (L2) of the sun-earth system.
2. Responsibility
The PLATO was selected by the Science Programme Committee (SPC) at its 143rd
meeting (ESA/SPC(2014)6) and adopted by the SPC during its 154th meeting in June 2017 (ESA/SPC(2017)10).
ESA has the overall responsibility for the PLATO mission design and implementation including the procurement of the launch service.
The scientific payload of PLATO will be developed and provided by a European scientific consortium (the PLATO Mission Consortium). The scientific payload consists of 26 FM Cameras, with Charge Coupled Devices (CCDs) as detection elements that are procured by the Agency, in their focal planes. The scientific payload is complemented by the associated digital and analogue electronics.
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The industrial Prime contractor is responsible for the Design, Development (including procurement, manufacturing, assembly, integration, test and verification) and Support to Launch and Post Launch Operations (Phase B2/C/D/E1) of the PLATO Spacecraft accommodating the delivered payload .
3. The Industry Day
Further to the Invitation To Tender (ITT) released by the European Space Agency (ESA) in July 2017, OHB System AG (Germany) has been selected as Prime Contractor of the PLATO space segment for the Implementation phase (B2/C/D/E1).
Therefore OHB has been authorized to proceed with the “Best Practices” 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 advance to the announcement on EMITS of the ITTs, the objective of the PID is to present to the European industry the overall PLATO mission, the associated business opportunities, the bidding process and schedule for the build-up of the PLATO spacecraft industrial team.
Registration details for participation will be published in the coming weeks.
For logistic reasons the participation is limited to 200 people with a maximum of 3 participants per company.
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4. Preliminary Agenda
Day 1
Part I: Plenary session – ESTEC Newton meeting room
9:00 – Visitors entrance and registration
9:30 – ESA presentation
Introduction : objectives & organization of the PID (ESA) PLATO mission (ESA) PLATO System and Space segment (ESA) PLATO programmatics (ESA) PLATO geographic return considerations (ESA) Procurement rules (Best practices, ESA and Industry roles) (ESA) About ECOS (ESA)
10:30 – OHB presentation
PLATO spacecraft (OHB) PLATO development logic : Models, objectives & schedule (OHB) PLATO industrial consortium procurement (OHB) The ITT Process (according to Best Practices) (OHB)
11:30 – Coffee break
12:00 – ITT presentation (OHB)
List and dates of the future ITTs (OHB) Presentation of each ITT (OHB)
12:45 – Logistics for the B2B (ESA)
13 :00 – Lunch
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Part II: Business 2 Business Splinters
14:00 – B2B (All)
17:00 – Day 1 Wrap-up (ESA)
Day 2
9:00 – Visitors entrance
9:30 – B2B (All)
12:45 – Day 2 Wrap-up (ESA)
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Attachment – Preliminary List of ITTs
Procurement Item Issuing Company ITT/RFQ issue
Service Module
Electrical & Power
Battery OHB 2020 Q1
SVM Harness SubSys OHB 2019 Q2
Communication
Communication SubSys OHB 2018 Q4
X-band Transponders COMMS lead
K-band Transmitters COMMS lead
K-band Travelling Wave Tube Amplifier COMMS lead
Antenna
Low Gain Antennas (LGAA) Kongsberg 2019 Q4
K-Band Signal Routing Assembly Kongsberg 2019 Q4
Antenna Reflector Assembly (ARA) Kongsberg 2019 Q4
Antenna TVAC tests Kongsberg 2019 Q4
Sun Shield and Solar Array
Sunshield / Solar Array SubSys OHB 2019 Q2
Photovoltaic Assembly SSH / SA lead
SSH Central Structure SSH / SA lead
Sunshield MLI SSH / SA lead
Sunshield Thermal Sensors SSH / SA lead
Sunshield Heaters SSH / SA lead
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Procurement Item Issuing Company ITT/RFQ issue
Hold-Down & Release Mechanisms SSH / SA lead
Sunshield Harness SSH / SA lead
Propulsion
CPPS SubSys OHB 2018 Q4
Reaction/Orbit Control Thrusters CPPS lead
Propellant Tank CPPS lead
Fill & Drain Valves CPPS lead
Propellant Latch Valve CPPS lead
Pressure Transducer CPPS lead
Propellant Filter CPPS lead
Thermal
SVM MLI OHB 2019 Q3
SVM Heaters OHB 2020 Q3
SVM Thermal Sensors OHB 2020 Q3
Structure
Central Tube S.A.B. Aerospace 2019 Q1
CFRP Panels S.A.B. Aerospace 2020 Q1
Radiator Panels S.A.B. Aerospace 2020 Q1
Machined Parts S.A.B. Aerospace 2020 Q1
SVM STR MGSE S.A.B. Aerospace 2020 Q1
Avionics
Payload Data Storage RUAG Sweden 2018 Q4
Software
ISVV SSF 2019 Q2
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Procurement Item Issuing Company ITT/RFQ issue
AOCS
High Performance Gyro TASinF 2019 Q2
Coarse Rate Sensor TASinF 2019 Q2
Attitude Anomaly Detector TASinF 2019 Q2
Sun Presence Sensor TASinF 2019 Q2
Reaction Wheels TASinF 2019 Q2
Star Tracker TASinF 2019 Q2
Accelerometers TASinF 2019 Q2
Payload Module
PLM Tertiary Structures OHB 2019 Q2
PLM Thermal Sensors OHB 2020 Q3
PLM Heaters OHB 2020 Q3
Service contracts
Mission Analysis OHB 2018 Q4
AIT Support S/C OHB 2020 Q4
Test Facility DMBB OHB 2018 Q4
Test Facility PLM OHB 2020 Q1
Test Facility S/C STM + PFM OHB 2021 Q2
Satellite Database OHB 2020 Q4
MGSE
MGSE Batch 1.1
Transport Container PLM-DMBB OHB 2018 Q4
Integration Base Frame PLM-DMBB OHB 2018 Q4
MGSE Batch 1.2
MGSE Test Rig for Payload Test OHB 2020 Q1
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Procurement Item Issuing Company ITT/RFQ issue
Multi-Purpose Trolley(+) PLM & S/C OHB 2019 Q1
Transport Container SVM & PLM OHB 2019 Q2
Vibration and Thermal Test Adapters PLM OHB 2019 Q2
Integration Base Frame and Lifting Device PLM OHB 2019 Q3
MGSE Batch 2
Multi-Purpose Trolley SVM & S/C OHB 2020 Q1
AIT Integration Stand Central & Avionics Module OHB 2020 Q1
Camera Handling Tool OHB 2020 Q2
Multi-purpose Assembly Plate OHB 2020 Q2
Payload Electronics Panel Tilt Trolley OHB 2020 Q3
Vibration, Acoustic and TVAC Adapters S/C OHB 2020 Q3
Lifting Device for Central Module & S/C OHB 2020 Q4
MPT Interface Ring & AIT Adapter S/C OHB 2020 Q4
AIT Clampband S/C OHB 2021 Q1
Lifting Device for PLM Mating with SVM OHB 2021 Q1
S/C Payload Electronics Panel Tilting Device OHB 2021 Q1
Transport Box AVM OHB 2021 Q3
Harness Support Structure for PLM Harness OHB 2022 Q1
De-Mating Support COM Panel OHB 2024 Q1
EGSE
EGSE Batch 1.1
Camera Thermal Control System EGSE OHB 2018 Q3
EGSE Batch 1.2
EPS Special Check-Out Equipment TASinUK 2019 Q2
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Procurement Item Issuing Company ITT/RFQ issue
CDMS Special Check-Out Equipment TASinUK 2019 Q2
TT&C Special Check-Out Equipment TASinUK 2019 Q2
TMTC Front-end electronics TASinUK 2019 Q2
EGSE Batch 2
RF Suitcase OHB 2021 Q4
OGSE
OGSE Batch 1.1
Alignment reference cubes OHB 2018 Q4
TED Test GSE batch 1.1 OHB 2018 Q4
TED Test GSE batch 1.2 OHB 2019 Q2
MGSE Test Rig for Payload Test OHB 2020 Q1
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