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GOES to the Pole Lars Peter Riishojgaard/UMBC & Dennis Chesters/NASA Geostationary-class...

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GOES to the Pole GOES to the Pole Lars Peter Riishojgaard/UMBC & Dennis Lars Peter Riishojgaard/UMBC & Dennis Chesters/NASA Chesters/NASA Geostationary-class meteorological imager in a Molniya Geostationary-class meteorological imager in a Molniya orbit orbit Busted forecasts do Busted forecasts do occur because occur because unobserved polar winds unobserved polar winds move into lower move into lower latitudes latitudes Polar cloud and water Polar cloud and water vapor features have vapor features have been tracked with been tracked with time-series satellite time-series satellite images in MODIS bands images in MODIS bands orbit is perfectly semi-geosynchronous orbit is perfectly semi-geosynchronous tric Kepler orbit ric Kepler orbit t 39750 km (geostationary orbit height ~36000 km) t 39750 km (geostationary orbit height ~36000 km) ht ~600 km ht ~600 km 63.4 degrees 63.4 degrees od ~11h 58m (half a sidereal day) od ~11h 58m (half a sidereal day) apogee w.r.t. Earth is fixed and stable! pogee w.r.t. Earth is fixed and stable! quasi-stationary imaging position near the apogee for about two thirds of the duration of the orbit uasi-stationary imaging position near the apogee for about two thirds of the duration of the orbit vely by USSR (to a lesser degree by the US) for communications purposes ely by USSR (to a lesser degree by the US) for communications purposes ted for meteorological applications by Kidder and Vonder Haar (1990) ed for meteorological applications by Kidder and Vonder Haar (1990) Polar (>60N) coverage Polar (>60N) coverage eliminates the high eliminates the high latitude gap in latitude gap in satellite-determined satellite-determined global winds global winds Low-risk mission at PDR level Low-risk mission at PDR level Science Team Science Team Lars Peter Riishojgaard, UMBC, PI Lars Peter Riishojgaard, UMBC, PI Bob Atlas, NOAA, Simulation/impact experiments Bob Atlas, NOAA, Simulation/impact experiments Dennis Chesters, GSFC, Instrumentation, mission Dennis Chesters, GSFC, Instrumentation, mission Ken Holmlund, EUMETSAT, Algorithm development Ken Holmlund, EUMETSAT, Algorithm development Jeff Key, NESDIS/ORA, Data processing, polar products Jeff Key, NESDIS/ORA, Data processing, polar products Stan Kidder, CIRA, High-latitude applications Stan Kidder, CIRA, High-latitude applications Arlin Krueger, UMBC, Volcano monitoring Arlin Krueger, UMBC, Volcano monitoring Paul Menzel, NESDIS/ORA, Cloud applications Paul Menzel, NESDIS/ORA, Cloud applications Jean-No Jean-No ël Thépaut, ECMWF, Global NWP applications ël Thépaut, ECMWF, Global NWP applications Chris Velden, CIMSS/UW, Algorithm development Chris Velden, CIMSS/UW, Algorithm development Tom Vonder Haar, CIRA, Satellite meteorology Tom Vonder Haar, CIRA, Satellite meteorology Lifetime Lifetime 36 months (60 month goal) 36 months (60 month goal) Orbit Orbit 718 min Molniya @ 63.4 degree inclination 718 min Molniya @ 63.4 degree inclination Visible channel Visible channel 0.55-0.88 micron @ 1 km resolution 0.55-0.88 micron @ 1 km resolution Infrared channels Infrared channels 3.9, 6.3, 7.1, 11.0, 12.0 microns @ 2 km 3.9, 6.3, 7.1, 11.0, 12.0 microns @ 2 km resolution resolution Radiometric Radiometric precision precision Vis 500:1 SNR @ 100%, IR 0.2K @ 300K or 0.5K Vis 500:1 SNR @ 100%, IR 0.2K @ 300K or 0.5K @ 250 K @ 250 K Radiometric Radiometric accuracy accuracy Vis 6%, IR 1 K Vis 6%, IR 1 K Field of Regard Field of Regard >24 degrees + star field >24 degrees + star field Time for full- Time for full- disk image disk image <15 minutes <15 minutes Input power Input power <180W (including 20% contingency) <180W (including 20% contingency) Mass Mass <136 kg (including 30% contingency) <136 kg (including 30% contingency) GOES-like instrument characteristics GOES-like instrument characteristics
Transcript
Page 1: GOES to the Pole Lars Peter Riishojgaard/UMBC & Dennis Chesters/NASA Geostationary-class meteorological imager in a Molniya orbit Busted forecasts do occur.

GOES to the PoleGOES to the PoleLars Peter Riishojgaard/UMBC & Dennis Chesters/NASALars Peter Riishojgaard/UMBC & Dennis Chesters/NASA

Geostationary-class meteorological imager in a Molniya orbitGeostationary-class meteorological imager in a Molniya orbit

Busted forecasts do occur Busted forecasts do occur because unobserved polar because unobserved polar winds move into lower latitudeswinds move into lower latitudes

Polar cloud and water vapor Polar cloud and water vapor features have been tracked features have been tracked

with time-series satellite with time-series satellite images in MODIS bandsimages in MODIS bands

•Molniya orbit is perfectly semi-geosynchronousMolniya orbit is perfectly semi-geosynchronous•Highly eccentric Kepler orbit Highly eccentric Kepler orbit

–Apogee height 39750 km (geostationary orbit height ~36000 km)Apogee height 39750 km (geostationary orbit height ~36000 km)–Perigee height ~600 kmPerigee height ~600 km–Inclination 63.4 degreesInclination 63.4 degrees–Orbital period ~11h 58m (half a sidereal day)Orbital period ~11h 58m (half a sidereal day)

•Location of apogee w.r.t. Earth is fixed and stable!Location of apogee w.r.t. Earth is fixed and stable!•Platform in quasi-stationary imaging position near the apogee for about two thirds of the duration of the orbitPlatform in quasi-stationary imaging position near the apogee for about two thirds of the duration of the orbit•Used extensively by USSR (to a lesser degree by the US) for communications purposesUsed extensively by USSR (to a lesser degree by the US) for communications purposes•First suggested for meteorological applications by Kidder and Vonder Haar (1990)First suggested for meteorological applications by Kidder and Vonder Haar (1990)

Polar (>60N) coverage eliminates Polar (>60N) coverage eliminates the high latitude gap in satellite-the high latitude gap in satellite-

determined global windsdetermined global winds

Low-risk mission at PDR levelLow-risk mission at PDR level

Science TeamScience Team•Lars Peter Riishojgaard, UMBC, PILars Peter Riishojgaard, UMBC, PI•Bob Atlas, NOAA, Simulation/impact experimentsBob Atlas, NOAA, Simulation/impact experiments•Dennis Chesters, GSFC, Instrumentation, missionDennis Chesters, GSFC, Instrumentation, mission•Ken Holmlund, EUMETSAT, Algorithm developmentKen Holmlund, EUMETSAT, Algorithm development•Jeff Key, NESDIS/ORA, Data processing, polar productsJeff Key, NESDIS/ORA, Data processing, polar products•Stan Kidder, CIRA, High-latitude applicationsStan Kidder, CIRA, High-latitude applications•Arlin Krueger, UMBC, Volcano monitoringArlin Krueger, UMBC, Volcano monitoring•Paul Menzel, NESDIS/ORA, Cloud applicationsPaul Menzel, NESDIS/ORA, Cloud applications•Jean-NoJean-Noël Thépaut, ECMWF, Global NWP applicationsël Thépaut, ECMWF, Global NWP applications•Chris Velden, CIMSS/UW, Algorithm developmentChris Velden, CIMSS/UW, Algorithm development•Tom Vonder Haar, CIRA, Satellite meteorologyTom Vonder Haar, CIRA, Satellite meteorology

Science TeamScience Team•Lars Peter Riishojgaard, UMBC, PILars Peter Riishojgaard, UMBC, PI•Bob Atlas, NOAA, Simulation/impact experimentsBob Atlas, NOAA, Simulation/impact experiments•Dennis Chesters, GSFC, Instrumentation, missionDennis Chesters, GSFC, Instrumentation, mission•Ken Holmlund, EUMETSAT, Algorithm developmentKen Holmlund, EUMETSAT, Algorithm development•Jeff Key, NESDIS/ORA, Data processing, polar productsJeff Key, NESDIS/ORA, Data processing, polar products•Stan Kidder, CIRA, High-latitude applicationsStan Kidder, CIRA, High-latitude applications•Arlin Krueger, UMBC, Volcano monitoringArlin Krueger, UMBC, Volcano monitoring•Paul Menzel, NESDIS/ORA, Cloud applicationsPaul Menzel, NESDIS/ORA, Cloud applications•Jean-NoJean-Noël Thépaut, ECMWF, Global NWP applicationsël Thépaut, ECMWF, Global NWP applications•Chris Velden, CIMSS/UW, Algorithm developmentChris Velden, CIMSS/UW, Algorithm development•Tom Vonder Haar, CIRA, Satellite meteorologyTom Vonder Haar, CIRA, Satellite meteorology

LifetimeLifetime 36 months (60 month goal)36 months (60 month goal)

OrbitOrbit 718 min Molniya @ 63.4 degree inclination718 min Molniya @ 63.4 degree inclination

Visible channelVisible channel 0.55-0.88 micron @ 1 km resolution0.55-0.88 micron @ 1 km resolution

Infrared channelsInfrared channels 3.9, 6.3, 7.1, 11.0, 12.0 microns @ 2 km resolution3.9, 6.3, 7.1, 11.0, 12.0 microns @ 2 km resolution

Radiometric precisionRadiometric precision Vis 500:1 SNR @ 100%, IR 0.2K @ 300K or 0.5K @ 250 KVis 500:1 SNR @ 100%, IR 0.2K @ 300K or 0.5K @ 250 K

Radiometric accuracyRadiometric accuracy Vis 6%, IR 1 KVis 6%, IR 1 K

Field of RegardField of Regard >24 degrees + star field>24 degrees + star field

Time for full-disk imageTime for full-disk image <15 minutes<15 minutes

Input powerInput power <180W (including 20% contingency)<180W (including 20% contingency)

MassMass <136 kg (including 30% contingency)<136 kg (including 30% contingency)

VolumeVolume <0.9 m X 1.2 m X 1.3 m<0.9 m X 1.2 m X 1.3 m

GOES-like instrument characteristicsGOES-like instrument characteristics

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