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Jason-3 Information Briefing -2013 Walid Bannoura Jason-3 Project - PowerPoint PPT Presentation

Jason-3 Information Briefing -2013 Walid Bannoura Jason-3 Project Manager NOAA NESDIS 1 Mission Overview Science Measurements Global sea surface height to an accuracy of < 4 cm every 10 days, for determining ocean circulation, climate


  1. Jason-3 Information Briefing -2013 Walid Bannoura Jason-3 Project Manager NOAA NESDIS 1

  2. Mission Overview Science Measurements Global sea surface height to an accuracy of < 4 cm every 10 days, for determining ocean circulation, climate change and sea level rise Mission Objectives • Operational ocean altimetry mission to enable the continuation of multi-decadal ocean topography measurements achieved through TOPEX/Poseidon, Jason-1 and OSTM/Jason-2 • NOAA and EUMETSAT are lead agencies with CNES and NASA/JPL providing implementation support Instruments* Mission Overview • Core Mission: • Launch Date: July 2015 (Re-planned) • Poseidon-3B Altimeter • Launch Vehicle: Falcon-9 • DORIS (Precise Orbit Determination System) • Proteus Spacecraft Bus provided by CNES • Advanced Microwave Radiometer (AMR) • Mission life of 3 years (goal of 5 years) • GPS Payload (GPSP) • 1336 km Orbit, 66º Inclination • Laser Retro-reflector Array (LRA) • Passengers (Experiments): • JRE (Carmen3 + LPT) NOAA funded items in BLUE * Same Requirements, S/C Bus, and orbit as Jason-2. Implementation approach is to maximize recurrence 2

  3. Jason Altimetry Applications & End Users High Wave Forecasting • Near real-time operational Operational Ocean oceanography: high wave “Weather”- 3-13 Feb 14 warnings, search & rescue, hurricane intensity forecasting • Season/Inter-annual: El Niño/La Niña forecasting Coast Guard Search & Rescue • Climate: continuity of 20+ year Jason sea level rise record Hurricane Intensity Global & Regional El Niño/La Oil Spill Monitoring Forecasting Sea Level Rise Niña Forecasting 3

  4. Jason-3 Mission Roles • EUMETSAT activities: • NOAA activities: – Project Management – Project Management – Ground System & Operations – Ground System & Operations * • Earth Terminal (1) • Satellite Operations Control Center (SOCC) • NRT product processing, archiving and distribution • CDA Stations (2) • Ground network • NRT product processing – User interface • All product distribution • All archiving • CNES activities: • Ground network – Project Management • Satellite operations after handover – Satellite, Proteus bus – User interface – Payload (on Behalf of EUMETSAT) • Nadir Altimeter POS3B * Modernizing the existing NOAA Jason-2 Ground Segment to • DORIS serve both Jason-2 and Jason-3 satellites – Joint Radiation Experiment Payload • CARMEN3 – LPT (Passenger –Experimental) • NASA activities: (On Behalf of NOAA) – Ground System & Operations – Project Management • Satellite Control Command Center (CCC) • OFL product processing and distribution – Launch vehicle • All archiving – Payload • Ground network • Satellite Operations before handover • Advanced Microwave Radiometer (AMR) • Navigation, Guidance, Expertise for all mission • GPS Receiver (GPSP) • Laser Retro-reflector Array (LRA) – System integration & test – JPL Payload integration and test – Mission Operation support for CNES – Mission Operation support for JPL instruments instruments – System Coordination for all mission phases – User interface 4

  5. Jason-3 Instruments Payload Provided Description By EUMETSAT Poseidon-3B A radar altimeter. The mission's main instrument. Measures sea level, wave heights and wind speed. Altimeter NOAA Advance Measures water vapor content in the atmosphere so Microwave that we can determine how it impacts radar signal Radiometer propagation (AMR) GPS Payload NOAA Tracking system that uses GPS constellation of satellites receiver (GPSP) to determine exact position of a transmitter. Enhances the Precise Orbit Determination (POD) performance of DORIS and LRA Laser Reflector NOAA Allows the spacecraft to be tracked with centimeter Array (LRA) accuracy by 40 satellite laser ranging stations Doris Tracking EUMETSAT Provides Precise Orbit Determination (POD). Locates the Receiver satellite on orbit in real time Joint Radiation CNES/JAXA Includes Carmen-3 (radiation and particle detectors) Experiment and Light Particle Telescope (LPT). Used to measure the (JRE) influence of space radiation on advanced components (Passenger - Experimental) NOAA funded items are in blue 5

  6. Jason-3 System elements GPSP Antenna U.S. Elements European Elements AMR Reflector AMR Electronics DORIS Poseidon 3B EUMETSAT – Usingen, Germany Altimeter NOAA - Wallops/ Fairbanks – Operational product Barrow - USA Dedicated Launch processing & Vehicle : Falcon9 v 1.1 Distribution LRA S/C Operations NOAA EUMETSAT (Suitland, MD) Science data Operational product processing, archive & processing and Science S/C Operations Distribution Data archive & CNES (Toulouse, Distribution France) NASA/JPL Passengers Ops NASA Instrument and mission Ops centers CNES- JAXA 6

  7. Spacecraft Status Spacecraft: Jason-3 spacecraft development is complete Spacecraft is in storage. - Pre-Ship review May 12, 2015 - Satellite Shipment to the launch site is early June 7

  8. Launch Vehicle Status • SpaceX achieved multiple successful launches with the new Falcon-9 Version 1.1 – Falcon-9 Version 1.1 scheduled to launch the Jason-3 spacecraft from Vandenberg AFB on July 22, 2015 8

  9. Ground System Status • CNES, EUMETSAT, NOAA, JPL – All 4 partner ground systems are implemented and validated • CNES Control Center and Mission Center SSALTO • EUMETSAT Processing Center and Usingen2 Earth terminal • NOAA Control Center, Stations and Processing Center • JPL Instrument Data system (IDS) and Radiometer Calibration system (ARCS) • Successfully completed all Technical Qualification Testing with all partners • Continue to conduct Operational Qualification Tests – First Launch Dress Rehearsal was completed successfully in March 2015 9

  10. Mission phases Phase Spacecraft activities Leader 3-5 days: LEOP CNES w/ support of LEOP S/C & instruments functional (nom/nom mode) EUMETSAT, NASA, NOAA 4 weeks max: Orbit acquis CNES w/ support of Orbit acquisition key point ASSESSMENT EUMETSAT, NASA, S/C on final orbit – Jason2 & 3 formation flight NOAA Jason-2 Orbit Change Jason2 & 3 tandem flight 2 months: Assessment In Flight Assessment meeting Fully assessed S/C on final orbit S/C & GS nominal operations 2 months max CNES w/ support of OPERATIONAL EUMETSAT, NASA, NOAA HandOver review S/C Operations Handed Over to NOAA NOAA w/ support of EUMETSAT, NASA, CNES Till S/C decommissioning Phase Leader Products activities Start of cycle CNES & NASA VERIFICATION w/ support of NOAA, 1 5 months max: NRT Verif First verif workshop EUM and PIs Jason2 & 3 formation Jason-2 / 3 Inter Calibration Key Point flight Final verif workshop 10 months max: OFL Verif OFL products reprocessing NRT products generation & dissemination OPERATIONAL EUMETSAT & NOAA Till S/C decommissioning OFL products generation CNES Till S/C decommissioning OFL products dissemination CNES & NOAA Till S/C decommissioning 10

  11. Products Web sites for Jason-3 • On CNES side, archiving and dissemination of offline Jason-3 products via: – AVISO CNES Data Center http://aviso-data-center.cnes.fr/ssalto – AVISO offline data user satisfaction survey performed each year • On NOAA side , archiving and dissemination of Jason-3 products via: – NODC: http://www.nodc.noaa.gov/SatelliteData/jason/ for NRT OGDR, IGDR and GDR as well as Quality Monitoring – CLASS: www.class.noaa.gov for telemetry, all auxiliary and ancillary data, and the XDGR family (with 4-6 hour latency). – GTS: Global Telecommunication System (alternative option for reception of BUFR products) • On EUMETSAT side, archiving and dissemination of J3 near-real-time products via: – The Earth Observation Portal available on www.eumetsat.int (retrieval of archived products). – EUMETCast: Satellite Broadcasting System (reception of disseminated products). – GTS: Global Telecommunication System (alternative option for reception of BUFR products). 11

  12. Summary • Jason-3 spacecraft development is complete – Spacecraft is in storage. Pre-Ship review May 12, 2015 • Ground System Status – All ground systems developments and tests are complete – Ground System Operational Qualification (QO) will continue through launch • First Launch Rehearsal (RG1) for GS was completed successfully in March • Launch Vehicle Development and Certification continue to be on the critical path • On target to launch Jason-3 spacecraft on July 22, 2015 12

  13. Back Up 13

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