EarthCARE. Projekt-Status und Möglichkeiten der Zusammenarbeit. Name: Uwe Slansky. DLR - Raumfahrt-Industrietage in Friedrichshafen 13./14.
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1 EarthCARE Projekt-Status und Möglichkeiten der Zusammenarbeit Name: Uwe Slansky DLR - Raumfahrt-Industrietage in Friedrichshafen 13./14. Mai 2009
2 EarthCARE System Definition 19/12/2006 Page 2
3 EarthCARE Programmatic Aspects Core TEAM / Industrial Consortium Work Share EarthCARE Prime Contractor Astrium GmbH Project Office System Engineering & Satellite AIV Avionics ESSS & ECGP for ECEESIM CPR I/F Engineering & Procurement Support Launcher & GS I/F Platform Equipment Avionics PCDU Battery CDMS S,X-Band EGSE OGSE On-Board S/W ISVV ECGP, ESSS Spacecraft Base Platform Astrium Ltd PF Engineering & AIT Mission Analysis Base Platform Equipment Structure Thermal HW Propulsion SS Solar Array Harness MGSE FGSE BBR Instrument SEA Ltd Engineering & AIT BBR Engineering Rutherford Applleton Lab. BBR Equipment Opto.-mechan. & thermal H/W Electrical H/W GSE ESSS Support ATLID Instrument Astrium SAS Engineering & AIT Laser Transmitter Galileo Avionica ATLID Equipment Opto.-mechan. & thermal H/W Optical Assembly Mechanisms Detector Assembly Electrical H/W GSE ESSS Support MSI Instrument SSTL Ltd Engineering & AIT VNS Camera Assembly TNO MSI Equipment Optical Bench Module Electrical H/W GSE ESSS Support 19/12/2006 Page 3
4 EarthCARE Mission Objectives Overview Radiation Budget Short Wave Long Wave Top of Atmosphere Reflection Absorbtion Reflection Absorbtion Emission Emission Cloud base height Precepitation Cloud top height Change in cloud amount, liquid and ice water content, effective radius, convective updraft and ice fall speed Convection Condensation Evaporation of Water Water Free Atmosphere Planetary Boundary Layer Earth Surface 19/12/2006 Page 4
5 EarthCARE System Definition Payload Composition and Mission Objectives 19/12/2006 Page 5
6 EarthCARE System Definition View Geometry ATLID 335nm (15ns) BBR 200nm 50μm MSI 670nm 12μm CPR JAXA active Radar at 94GHz P Peak 1,8kW (3,3 μs) 10 km x 10 km GSD < 10 km < 30 m GSD < 200m Goal 100m 19/12/2006 Page 6 CPR < 1 km GSD 0.5 km averaging < 500 m flight direction BBR Forward view BBR Nadir view BBR Backward view m x 500 m GSD < 500 m Swath >150 km (35 km / 115 km) Yaw stering < +/
7 EarthCARE Satellite Overall Configuration +X- Flight CPR Antenna (Ø 2.50m) +Z- Nadir 6.0 m Solar Array Stack ATLID 1.1 m CPR Support Structure 18.5 m S/X-BAND 1.2 m Thrusters BBR MSI 1.8 m 1.6 m EarthCARE Satellite Equipment & Instrument Accommodation 19/12/2006 Page 7
8 EarthCARE System Definition Model Philosophy Platform SM Instrument SMs Spacecraft SM Platform PFM Instrument PFMs Spacecraft PFM Structural Model EarthCARE Spacecraft Model Philosophy Proto-Flight Model Electrical Functional Model Platform EM Units Instrument EMs Electrical Functional Model 19/12/2006 Page 8
9 EarthCARE Overall Schedule 19/12/2006 Page 9
10 EarthCARE Programmatic Aspects The European Space Agency (ESA) has contracted Astrium GmbH for the delivery of the EarthCARE satellite and for additional system activities regarding launch campaign and in orbit commissioning. Astrium GmbH has teamed with Astrium Ltd for the base platform, Astrium SAS for the ATLID instrument, SSTL for the MSI instrument and SEA for the BBR instrument. The procurement and especially the selection of subcontractors will run under ESA's supervision in accordance with the Best practices for the Selection of Subcontractors, tailored to the needs of the EarthCARE contract. Procurement will commence after the System Requirements Review (SRR). Specific announcement of intended ITT will be published on EMITS approximately four weeks in advance to the proper ITT. 19/12/2006 Page 10
11 Zukünftige Aktivitäten PT No. Procurement Item Procurement Method ITT Issuing Company ITT tentative date 1112 SiC Mirrors polishing & coating 1113 Isostatic Mounts, Fixations &Covers ATLID Structure Emit & Receive Optics Fibre Coupler Assembly Laser Chopper Mechanism Instr, Detection Electronics ACDM ATLID Harness Test Facilities ICU and Harness Main Structure CPR Support Structure PF SM Mass dummies per H/W item SSTL 19/12/2006 Page 11
12 Zukünftige Aktivitäten PT No. Procurement Item Procurement Method ITT Issuing Company ITT tentative date 2200 Spacecraft Harness Q4/ Solar Array (incl. HDRM, photovoltaic & substrates) Thermal Control H/W Tank Valves Thrusters, Pipework, Propellant MGSE for Satellite GPS Assembly (incl. GPS Sim ) Mass Memory & Formatting Unit X-Band Transmitter Platform Interface Simulator Assembly ECGP ASD ASD ASD ASD ASD 19/12/2006 Page 12
13 EarthCARE Ansprechpartner Projektleiter Uwe Slansky, Systemingenieur Michael Gotsmann, Procurement Wolfgang Rühe, /12/2006 Page 13
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