ASI EO Info Day October Rome
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1 ASI EO Info Day October Rome Danilo Muzi 18/10/2012
2 EE Missions Overview Contents: Swarm ADM Aeolus EarthCARE ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 2
3 ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 3
4 Swarm Scientific Objectives Objectives: the Earth Studies of core dynamics, geodynamo processes, and coremantle interaction, Mapping of the lithospheric magnetisation and its geological interpretation, Determination of the 3-D electrical conductivity of the mantle, Identifying the ocean circulation by its magnetic signature Objectives: near-earth Electromagnetic Environment Investigation of electric currents flowing in the magnetosphere and ionosphere, Quantifying the magnetic forcing of the upper atmosphere correction Resolution Magnetic field magnitude and vector components (0,3 nt magnitude, 1 nt vectorial) Electric field vector components (10 mv/m) ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 4
5 Swarm Constellation Constellation of three identical satellites Two orbit side-by- side, decaying naturally from an initial altitude of 460 km to 300 km over 4 years The third maintains an altitude of about 530 km The inclination difference of 0.6 between the lower pair and the higher satellite ensures a 90 difference in orbital plane by the third year of operations ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 5
6 Swarm Project Status Satellites AIT program is finalised. All system tests have been completed. Satellite Flight Acceptance Review (FAR) has been completed. Pre-Shipment Review (PSR) held in September Satellites and GSE are in their transport containers, ready to be shipped to the launch site. Ground Segment Ground Segment Acceptance Review (GS-AR) completed. Ground Segment Overall Verification (GSOV) completed. Simulation campaigns at ESOC will start in December (operators training). Launch Vehicle Launcher Design Qualification Review (DQR) completed in July Scientific Community Validation Teams have been identified. First Validation workshop has been held in June Constellation of three identical satellites ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 6
7 Swarm Satellite Magnetic Characterisation at Magnetic Field Simulation Facility (IABG) 472kg incl. 106kg gas (freon) ~1.0 m² cross section; ~9m long ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 7
8 Swarm Instruments Absolute Scalar Magnetometer (CNES/Leti) ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 8 Vector Field Magnetometer and Star Tracker Assembly on Optical Bench (both instrument from DTU) Accelerometer (VZLU)
9 Swarm Instruments Electric Field Instrument (Com Dev) It is composed of 2 types of sensors: Thermal Ion Imagers (UoC) Langmuir Probes (IRFU) ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 9
10 Swarm Satellites - pictures Launcher adapter fit-check (IABG) ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 10
11 SWARM Launch The 3 Satellites are stored in the clean room in IABG - Munich since July 2012 Rockot Launch Vehicle with Breeze-KM Upper Stage Single Launch Simultaneous separation Integrated Adapter & Separation System WARM Launch Schedule Launch Campaign start: January/February 2013 Launch: March/April 2013 ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 11
12 ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 12
13 ADM AEOLUS: ESA s wind mission Scientific objectives Improve understanding of 1. Global atmospheric dynamics/transport 2. Global cycling of energy, water, aerosols and chemicals through improvements of model dynamics How are they achieved? 1. Improved representation of winds in atmospheric analysis, in particular: a. Tropics: Wind fields governs dynamics b. Mid-latitudes: Intense storm developments and mesoscale circulation systems Benefits Better initial conditions for weather forecasting Improved parameterisation of atmospheric processes in models Advanced climate and atmospheric flow modelling Demonstrate the capabilities of space-based Doppler Wind LIDARs for global wind profiling and its potential for operational use ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 13
14 Aladin measurement principle (= height) ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 14 Wind and atmospheric optical properties profile measurements are derived from the Doppler shifted signals that are back-scattered by aerosols and molecules along the lidar line-of-sight (LOS)
15 Summary of Status Satellite: all items are ready for satellite FM integration except the Aladin instrument and one panel of the platform where the In-Situ Cleaning System will be installed. Aladin instrument: 1. Transmit and Receive Optics (monostatic configuration)- completed Electronic Units completed Laser Transmitter (FMA, FMB and FMC) in integration/refurbishment 2. Test of the FM-A Laser transmitter under low pressure (40Pa) oxygen conditions has been completed, ~150 Million shots. Most of the test objectives have been successfully achieved, e.g. no Laser Induced Contamination detected, stable beam profile and position, controllable output energy. Unfortunately, unexpected small laser damage sites were found on the UV optics exposed to the highest energy densities. Extensive investigations are being carried out to identify causes and remedies Launch: July 2015 (VEGA/Verta Launcher) ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 15
16 Platform and Aladin Instrument ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 16
17 Aladin Laser Transmit Path ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 17
18 Laser Transmitter ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 18
19 ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 19
20 EarthCARE Objectives and Synergy EarthCARE has been defined with the specific scientific objectives of quantifying aerosol-cloud-radiation interactions so they may be included correctly in climate and numerical weather forecasting models. ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 20
21 Project Status and CDR Planning Project formally in Phase C/D and detailed Design phase on going Procurement process almost completed System CDR next year (Most Avionics and Electrical Units CDR already passed): Structure CDR Completed RCS CDR October 2012 Thermal CDR December 2012 ATLID Sub-systems CDR planned in Q1-Q CPR CDR planned end-2012 BBR CDR on going with planned close-out October 2012 MSI Instrument CDR K/O end-2012 GS-PDR planned in Q EarthCARE Electrical Functional Model testing on going Launch: November ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 21
22 EarthCARE Configuration ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 22
23 Laser Transmitter status Full laser chain breadboard validating the laser performance FM laser diodes manufactured Reference Laser Head manufacturing on-going First amplifier manufactured- Characterisation on-going Structural and thermal model of the pressurised housing under manufacture EQM assembly of the Power Laser Head planned from next year Beam expander design is being consolidated Fiber injection ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 23
24 Laser Transmitter status Pump Unit PLTM (Pressurized LIC test Model) Transmitter Breadboard Fiber injection Main Mirror ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 24
25 MSI Status ECM VNS Camera Delivery to SSTL in October 2012 VNS ECM TIR Camera Vibration Test Completed ICU EM testing on going Engineering Confidence Model Integration and test end-2012 Instrument CDR end-2012 Sun Baffle SWIR-2 radiator OB TIR Fiber injection ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 25
26 BBR Status All Flight Detectors delivered First telescope assembled and undergoing testing in NPL ICU EM Final Testing on going Instrument CDR on going with close-out in October 2012 Fiber injection ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 26
27 CPR Status CPR SM delivered in March 2012 to ESA for fit check purposes on PFM structure (not OK for system mechanical test) CPR Electrical Interface Simulator (CEIS) Delivery planned end-2012 for integration on Spacecraft EFM (Electrical, Software and Operational Interfaces) CPR Engineering Model Testing on going in Japan CPR Instrument CDR end-2012 ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 27
28 Electrical Functional Model ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 28
29 Thank you for your attention! European Space Agency - ESTEC ASI Info Day Danilo Muzi 18/10/2012 EOP Slide 29
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