NOAA Plans for LEO & GEO The long and winding road from TOVS to NPOESS and ATS to ABS Paul Menzel NOAA/NESDIS/ORA TOVS, ATOVS, MODIS, AIRS, VIIRS, CrIMSS ATS, SMS, VISSR, METEOSAT, VAS, GOES, GHIS, GIFTS, ABS Anticipated Capabilities
Long Range Integrated Satellite Transition CY Local Equatorial Crossing Time DMSP POES Aqua C2 or C1 DMSP POES NPP Terra METOP WindSat 19 GEO GIFTS POLAR GIFTS/IOMI GOES – R Series Integrated System NPOESS GOES
POES (K-N`) Instruments AVHRR HIRS SARR
Orbit type (equatorial crossing times) Future Additional Satellites Operator launch date Other information “Morning” (6:00 – 12:00) (18:00 – 24:00) NOAA-M NPOESS-1 NPOESS-4 NOAA 6/ (9:30) Sun-synchr. “Afternoon” (12:00 – 16:00) (00:00 – 04:00) NOAA-N NOAA-N’ NPOESS-2 NPOESS-5 NOAA 6/2004 3/ (13.30) “Early morning” ( 4:00 - 6:00) (16:00 – 18:00) DMSP-S16 DMSP-S17 DMSP-S18 DMSP-S19 DMSP-S20 NPOESS-3 NPOESS-6 NOAA (5:30) Planned Leo Launches
New environmental remote sensing capabilities are offering higher spatial resolution more spectral bands higher spectral resolution higher temporal resolution better calibration better science Synergy is increasing between POES and GOES sensors research and operational sensors US and international sensors Opportunities can be realized with new approaches new partnerships early involvement in science teams and associated field programs land ocean atmosphere weather climate VIS IR MW active passive
NPOESS Instruments US 0530US 0930US 1330EUM 0930 VIIRSVIIRSVIIRS CMISCMISCMIS CrISIASI ATMSAMSU/MHS OMPSGOME GPSOSGPSOSGRAS SESSSESSSEM CERES TSIS ALT ASCAT DCSDCSDCS SARSATSARSATSARSAT
VIIRS, MODIS, FY-1C, AVHRR H2O O2 CO2 H2O O2 O3 H2O O2
FY-1C AVHRR MODIS plus more IR VIIRS M M M M I M M M I M M M I M M I M M M M I Spectral bands of polar imagers (nm or um)
Earth emitted spectra overlaid on Planck function envelopes MODIS VIIRS
II II I |I IATMS Spectral Regions
NPOESS Instruments in Development/Production Phase Ozone Mapping & Profiler Suite (Artist Conception) Ball Advanced Technology MW Sounder (ATMS) (GSFC Notional Design) Aerojet Cross-track IR Sounder (CrIS) (Engineering Development Unit) ITT Visible/IR Imaging Radiometer Suite (VIIRS) (Artist Conception) SBRS 176 kg 170 W 10.5 Mbps 87 kg 91 W 1.8 Mbps 45 kg 45 W 180 kbps 66 kg 85 W 30 kbps
NPP PROPOSED INSTRUMENTS FROM IPO VIIRS (VISIBLE INFRARED IMAGER RADIOMETER SUITE) 21 CHANNELS (INCLUDING.4,.5,.6,.7,.8,.9, , 1.6, 2.3, 3.7, 8.6, 10.3, 11.0, 12.0 UM) 12 BIT, 0.8 KM RES, VIS CAL, IRW NEDT OF.1 K CRIS (CROSS TRACK IR SOUNDER) INTERFEROMETER COVERING SW (4.0 UM) TO LW (15.4) 1 KM (VERT), ~10 KM (HOR), AND 1 K RES LEVERAGED FROM NASA ATMS (ADVANCED TECHNOLOGY MICROWAVE SOUNDER) COVERING 23, 31, 50, 57, 89, 166, AND 183 GHZ BANDS 10 KM FOV AT 183, S/N AS GOOD AS AMSU IN CRIS FOV, 118 GHZ ALSO BEING EXPLORED
Suggested ATMS Channels Ch (GHz)BW(GHz)Characteristic 1* split window-water vapor 100 mm 2* split window-water vapor 500 mm 3* window-surface emissivity window-surface emissivity 5* surface air 6*53.596± km ~ 700 mb temp and precip 7* km ~ 400 mb temp and precip 8* km ~ 250 mb 9* km ~ 180 mb 10* km ~ 90 mb 11* ± km ~ 50 mb 12* ±.322 ± km ~ 25 mb 13* ±.322 ± km ~ 10 mb 14* ±.322 ± km ~ 6 mb 15* ±.322 ± km ~ 3 mb 16* window-precip and water vapor 150 mm H 2 O 18 mm 18*183.31±72.0H 2 O 8 mm ±4.52.0H 2 O 4.5 mm 20*183.31±31.0H 2 O 2.5 mm ±1.81.0H 2 O 1.2 mm 22*183.31±10.5H 2 O 0.5 mm * In common with AMSU/HSB
GOES Satellites Imager 120 kg 177 W 2.62 Mbps Sounder 132 kg 178 W 40 kbps GOES-I Series 2105 kg GOES-N Series 1615 kg SXI 23 kg 57 W 100 kbps IOO 35 kg 150 W 100 kbps
Sector Future additional satellites operator Planned launch ( Planned location) Other remarks E-Pacific (180°W- 108°W) and West Atlantic (108°W- 36°W) GOES-N GOES-O GIFTS GOES-P GOES-R NOAA NASA/ NOAA 4/ ° or 75° W 135°,100 °, 75° W, then Indian Ocean 135° or 75° W Planned Geo Launches
"Normal people... believe that if it ain't broke, don't fix it. Engineers/Scientists believe that if it ain't broke, it doesn't have enough features yet."
ABI addresses the NWS Imager concerns by: - increasing the spatial resolutions (the NWS goal is 0.5 km for the IR) - improving temporal sampling (faster scanning plus more regions scanned) - adding spectral bands (enables new and/or improved products) A view into the future: simulations of improved cloud, moisture, and surface products with ABI. Advanced Baseline Imager on GOES-R
Two visible bands, two near IR and eight IR bands (10.3 not shown) Simulated ABI (from MODIS) All images are displayed at 2 km resolutions
Simulated GOES (from MODIS) All images are displayed at 2 km resolutions One visible (at a higher resolution) band and four IR bands
Lake Effect Snow Bands: Visible January 19, :15 UTC MODIS 0.25 km MODIS 0.5 kmActual GOES-8 1 km MODIS 0.25 km
MODIS 1 km MODIS 0.5 km Ice On Lake Erie: Visible February 12, :27 UTC 0.25 km data represents possible future (beyond ABI) GOES visible imagery. MODIS 0.25 km
ABI Simulations (from MODIS data) Water/Ice Clouds and Snow/Lake Ice 3-color composite (Visible/1.6 μm/ μm) February 12, :27 UTC UW/CIMSS Vis/1.6um/8.5-11um Water cloud Ice cloud Lake Ice Snow Super-Cooled cloud UW/CIMSS
MODIS RGB composite shows one application of the 0.47 m on the ABI. UW/CIMSS
Advanced Baseline Sounder on GOES-R *Addresses NWS concerns by improving - temporal resolution: ‘sounding disk’ in 1 hour - vertical resolution 1 km for temp, 2 km for moisture - spatial resolution to 10 km for independent obs * Geo - Interferometer combines several advanced technologies - large focal plane detector arrays - Fourier Transform Spectrometry - on-board data processing. * ABS will provide moisture and cloud information as never before.
Areas within 62 degrees local zenith angle from GOES-East and GOES-West sub- satellite points are indicated. Threshold coverage rate calls for the 62 arc region, excluding half of over-lap, to be scanned each hour. Current GOES -E and -W sounder hourly coverage is also shown. Spatial Coverage UW-Madison/CIMSS
ABS’ using the shortwave side of the water vapor band.
The advanced sounder has more and sharper weighting functions UW/CIMSS These water vapor weighting functions reflect the radiance sensitivity of the specific channels to a water vapor % change at a specific level (equivalent to dR/dlnq scaled by dlnp). Moisture Weighting Functions Pressure Weighting Function Amplitude Wavenumber (cm-1)
NASA NMP
Geostationary Sounders (# of channels) VAS (experimental) GOES Sounder (operational) GIFTS (experimental) (12) (18) (~1600) Advanced Baseline Sounder (operational) time The ABS is the next logical step from experimental low spectral resolution to finally operational high-spectral resolution sounders.
Long Range Integrated Satellite Transition CY Local Equatorial Crossing Time DMSP POES Aqua C2 or C1 DMSP POES NPP Terra METOP WindSat 19 GEO GIFTS POLAR GIFTS/IOMI GOES – R Series Integrated System NPOESS GOES
Summary The satellite remote sensing capability has had many positive consequences: –it has saved thousands of lives and millions of dollars from the ravages of storms; –it has made meteorological satellite data routinely available to nations around the globe; –in conjunction with improvements in numerical weather prediction, it has helped to improve forecast skill significantly; –and as valuable part of GOS it will help discern climate trends. NOAA is investigating the opportunities for further evolving the geostationary and polar orbiting remote sensing capabilities:
Remote sensing of gradients in spectra, space, and time will be better than ever The business of looking down is looking up