MHS scans in the cross-track direction at a rate of 8/3 seconds (2.67 s) in continuous mode. NOAA POES Series - 5th Generation Satellites, Launch    Spacecraft    Sensor Complement - NOAA-15   Mission Status    Sensor Complement - POES   References. Electrons are measured in thee bands: >30 to > 300 keV. Attitude accuracy is 0.2º, knowledge is 0.1º in post-processing. 9) "NOAA-15 Makes 100 Thousandth Orbit," NOAA/NESDIS, Aug. 10, 2017, URL: https://www.nesdis.noaa.gov/content/noaa-15-makes-100-thousandth-orbit, 10) "POES Operational Status," April 16, 2016, URL: http://www.ospo.noaa.gov/Operations/POES/status.html, 11) "Ten years ago, on 20 May 2005, the first Microwave Humidity Sounder (MHS) instrument was launched into orbit on board the NOAA-18 satellite," EUMETSAT, May 20, 2015, URL: http://www.eumetsat.int/website/home/News/DAT_2645091.html, 12) "POES Operational Status," NOAA, Sept. 30, 2014, URL: http://www.ospo.noaa.gov/Operations/POES/status.html, 14) "NOAA 19 Spacecraft Status Summary," NOAA, June 2009, URL: http://www.oso.noaa.gov/poesstatus/spacecraftStatusSummary.asp?spacecraft=19, 15) NOAA KLM User's Guide, Instrument Payload (General Descriptions), URL: http://www2.ncdc.noaa.gov/docs/klm/html/c1/sec12-2.htm, 16) CEOS Summary Report, WGD-10 Meeting, Annapolis MD, April 16-18, 1991, 17) Information provided by G. A. Mandt of NOAA POES Program, "AVHRR/3 Instrument Technical Overview," March 15, 1995 of ITT A/CD, 18) http://www2.ncdc.noaa.gov/docs/klm/html/c3/sec3-1.htm, 19) D. Rosenfeld, E. Cattani, S. Melani, V. Levizzani, "Consideration on Daylight Operation of 1.6- versus 3.7-µm Channel on NOAA and MetOp Satellites," BAMS (Bulletin of the American Meteorological Society), Vol. Secondly, while the HIRS/3 is used primarily for temperature sounding, channel 20 has been upgraded to enhance generation of radiation budget products. The data samples are output in a non-continuous burst of 10 space samples, 2048 Earth samples, and 10 internal calibration target samples at 6 Hz, synchronized with the scan mirror. Note: With the launch of NOAA-M (NOAA-17, launch June 24, 2002) the equator crossing time of the AM series spacecraft was changed from 7:30 AM to 10:00 AM (on descending node). Extreme Ultraviolet and X-ray Irradiance Sensors (EXIS)​. • NOAA-16 (L): The spacecraft, with a launch Sept. 21, 2000, is in backup mode for the PM orbit. 0.25 - Digital to analog - The digitally processed APT data are converted to a 2080 Hz bandwidth analog signal, amplitude modulated onto a 2.4 kHz carrier, and bandwidth limited to 4160 Hz in preparation for transmission by the VHF transmitters.

Click here for more information about GLM. AVHRR/3 provides some data processing provided by MIRP (Manipulated Information Rate Processor). The PTT capacity was increased from four to eight, this means eight DRU (Data Recovery Unit) on-board. The instrument's IFOV is 1.1º and the separation between the center of one Earth view to the next is 1.1º. 1988 is collected and processed across the Weather Enterprise and then fed to the AWIPS Program Network Control Facility which disseminates the products via the AWIPS Satellite Broadcast Network (SBN) / NOAAPort data broadcast via the Galaxy 28 Satellite. 36 On April 3, 2020, NOAA’s National Environmental Satellite, Data, and Information Service (NESDIS) began awarding contracts for satellite mission and instrument design analysis. NOAA-15 also collects data from buoys and remote weather stations for the ARGOS (Advanced Research and Global Observation Satellite) program dedicated to environmental study and protection. The sensor scans across-track in a `stop-and stare' mode (discrete stepping) at a scan rate of 6.4 s (56 Earth views per scan). ABI is the primary instrument on the GOES-R Series for imaging Earth’s weather, climate, oceans and the environment. LTAN (LTAN values are valid as of April 19, 2016), Table 5: Overview of POES operational missions, • May 20, 2015: Four MHS instruments are currently on orbit (on Metop-A and -B and NOAA-18 and -19) and are in good health — the only exception being one channel on NOAA-19. 5 2000, 0.37 OBCT (Onboard Calibration Target) is a hot target comprising an array of RF (Radio Frequency) absorbent pyramids. Channel 11 on the AMSU-A instrument failed in April 2002. A silicon photodiode at the instrument temperature (nominally 15º C) detects the visible energy. In addition to providing high-resolution atmospheric moisture profiles, AMSU-B is used to produce precipitation and surface products from two window channels. AMSU is a 20-channel microwave radiometer.

It is a zero-momentum system consisting of reaction wheels and Earth, sun, and inertial reference sensors. There are three types of direct broadcasting: (1) the real-time HRPT, (2) the direct sounder broadcast (DSB), also referred to as the real-time very high frequency (VHF) beacon transmissions, and (3) the Automatic Picture Transmission (APT). This was done to improve the utility of the data near cloud boundaries.

H Objectives: atmospheric temperature profile measurements from the surface up to about 50 km in 15 channels. This sensor is used on PM and late AM missions [NOAA-17 (-M) is in a 10 AM descending sun-synchronous orbit. Banks, "An overview of the NOAA/NESDIS data processing systems and derived products for NOAA-KLM," Earth System Monitor, Vol. 2 x 1000 (dual side band) These are key inputs for numerical weather prediction models, which are used operationally for weather forecasting worldwide. Central Pacific Hurricane Center 2525 Correa Rd Suite 250 Honolulu, HI 96822 W-HFO.webmaster@noaa.gov

Weather data (satellite imagery, radar data, model data, sensor data, etc.) The spacecraft structure has been stiffened primarily to support the heavier AMSU instruments and improve launch vehicle load margins. Each antenna provides a cross-track scan of ±48.33º from nadir with a total of 30 contiguous Earth views (stepped scan positions) per scan line. The Magnetometer provides measurements of the space environment magnetic field that controls charged particle dynamics in the outer region of the magnetosphere. The instrument is providing a humidity profiling capability in the frequency range of 89 - 190 GHz. John Bateman Each sensor consists of a dome of moderating material which absorbs energy from the particle (and so sets the detection energy threshold), a silicon solid state detector, a preamplifier, and a level comparator which responds to particles with enough energy to go through the moderator and produce a pulse from the detector large enough to exceed the level in the comparator. DCS-2: From NOAA-K onwards (satellites and its successors, there is a modified Argos data collection system referred to as DCS-2 (the predecessor of A-DCS). MHS technology used: advanced quasi-optics, planar millimetric frontends, precision calibration target, scan mechanism and reflector are combined with low power and mass electronics for minimum mass and power. 7 20) 21), TIR: <1.5% of 1.8º step size; SWIR: <1% of cha. Figure 3: Simplified block diagram of ADACS (image credit: NOAA), Sun-synchronous circular, altitude = 833±19 km or 870±19 km, inclination = 98.7º (retrograde), 4.18 m length, 1.88 m diameter, overall length = 7.4 m, 1479 kg on orbit, 2232 kg at launch (756 kg propellant), 833 W min, array size: 2.73 m x 6.14 m (16.76 m2), 5 DTR (Digital Tape Recorder), each with a capacity of 0.9 Gbit. NOAA POES Series - 5th Generation Satellites . Information provided by SEISS is used for assessing radiation hazards to astronauts and satellites and to warn of high flux events, mitigating damage to radio communications. Calibration of the IR channels is performed with four internal blackbodies every scan line.17) 18), 20.3 cm diameter afocal reflective Cassegrainian type, 21 cm x 29.5 cm elliptical ribbed beryllium, Two stage radiant cooler controlled @ 105 K, 40 kHz simultaneous sample of all channels, 200 k word/s max (2 Mbit/s in burst mode, 621.3 kbit/s average), Table 7: AVHRR/3 performance characteristics, Night cloud mapping, sea surface temperature, Table 8: Spectral parameters of AVHRR/3 channels, AVHRR/3 adds a sixth channel in the IR range at 1.61 µm (referred to as channel 3a, operating during the daylight part of the orbit). 0.84 The basic intent is to join the space segment of the emerging MetOp program of EUMETSAT with the existing POES program of NOAA into a fully coordinated service, thus sharing the costs of a program for synergetic reasons.

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1000 0.4 SEM-2 is a multichannel, charged-particle spectrometer that measures the population of the Earth's radiation belts and the particle phenomena resulting from solar activity (both of which contribute to solar/terrestrial energy interchange). It was deactivated on June 16, 2004. The data from the six channels is simultaneously sampled at 40 kHz and converted to 10-bit binary values. Reduced resolution AVHRR data (4 km) plus stored TIP data at full resolution soundings. 1335 East-West Highway, SSMC1,  H Solid-State Recorders (SSR) will fly on NOAA-M (1 SSR, 4 DTR), and NOAA-N and NOAA-N' with 3 SSRs each with a capacity of 2.7 Gbit, Star 37XFP (Thiokol Corporation), used to circularize the orbit after S/C separation. The S&RSAT payload consists of S&RR (S&RSAT Repeater), provided by CRC/Canada; and S&RP (S&RSAT Processor), provided by CNES/France). The spacecraft transmits instrument data to the ground for three primary functions: Command and Data Acquisition (CDA), Direct Broadcast, and Search and Rescue (S&R). Two independent measurements of the particle energy flux are made at zero and 30 degrees from the local vertical. Today, the satellite serves as the back-up to EUMETSAT's Metop-B satellite, which provides data in the morning, and continues to serve as part of the SARSAT system, which as of July 31, 2017, assisted in the rescue of 158 people so far this year. • NOAA-19 (N'): The spacecraft, with a launch on Feb. 6, 2009, was declared "operational" by NOAA in June 2009. Dec. 30, 1994 For instance, NOAA-M, launched on June 24, 2002, was redesignated as NOAA-17 after achieving its sun-synchronous LEO (Low Earth Orbit). The observed swath width is ±1078 km. Channel 3b corresponds to the previous channel 3 on AVHRR/2 and operates during the night portion of the orbit. - "NOAA's careful operations and management of polar-orbiting satellites has resulted in over 19 years of operations for NOAA-15, far exceeding its planned five year lifetime," said Vanessa Griffin, Director of NOAA's Office of Satellite and Product Operations. AMSU-A utilizes an 8-second scan period with a step and settle scan across the Earth scene while AMSU-B utilizes an 8/3-second scan period with a constant speed scan across the Earth scene. The MetOp series will also use an X-band downlink for instrument data dumps from the on-board solid-state recorder. SBUV/2 (Solar Backscatter Ultraviolet Radiometer): SBUV/2 was developed by Ball Aerospace, Boulder, CO. SBUV/2 is a further development of SBUV flown on Nimbus. 90-θ The CDA stations receive stored GAC (Global Area Coverage) and LAC (Local Area Coverage) data from each spacecraft.

MHS scans in the cross-track direction at a rate of 8/3 seconds (2.67 s) in continuous mode. NOAA POES Series - 5th Generation Satellites, Launch    Spacecraft    Sensor Complement - NOAA-15   Mission Status    Sensor Complement - POES   References. Electrons are measured in thee bands: >30 to > 300 keV. Attitude accuracy is 0.2º, knowledge is 0.1º in post-processing. 9) "NOAA-15 Makes 100 Thousandth Orbit," NOAA/NESDIS, Aug. 10, 2017, URL: https://www.nesdis.noaa.gov/content/noaa-15-makes-100-thousandth-orbit, 10) "POES Operational Status," April 16, 2016, URL: http://www.ospo.noaa.gov/Operations/POES/status.html, 11) "Ten years ago, on 20 May 2005, the first Microwave Humidity Sounder (MHS) instrument was launched into orbit on board the NOAA-18 satellite," EUMETSAT, May 20, 2015, URL: http://www.eumetsat.int/website/home/News/DAT_2645091.html, 12) "POES Operational Status," NOAA, Sept. 30, 2014, URL: http://www.ospo.noaa.gov/Operations/POES/status.html, 14) "NOAA 19 Spacecraft Status Summary," NOAA, June 2009, URL: http://www.oso.noaa.gov/poesstatus/spacecraftStatusSummary.asp?spacecraft=19, 15) NOAA KLM User's Guide, Instrument Payload (General Descriptions), URL: http://www2.ncdc.noaa.gov/docs/klm/html/c1/sec12-2.htm, 16) CEOS Summary Report, WGD-10 Meeting, Annapolis MD, April 16-18, 1991, 17) Information provided by G. A. Mandt of NOAA POES Program, "AVHRR/3 Instrument Technical Overview," March 15, 1995 of ITT A/CD, 18) http://www2.ncdc.noaa.gov/docs/klm/html/c3/sec3-1.htm, 19) D. Rosenfeld, E. Cattani, S. Melani, V. Levizzani, "Consideration on Daylight Operation of 1.6- versus 3.7-µm Channel on NOAA and MetOp Satellites," BAMS (Bulletin of the American Meteorological Society), Vol. Secondly, while the HIRS/3 is used primarily for temperature sounding, channel 20 has been upgraded to enhance generation of radiation budget products. The data samples are output in a non-continuous burst of 10 space samples, 2048 Earth samples, and 10 internal calibration target samples at 6 Hz, synchronized with the scan mirror. Note: With the launch of NOAA-M (NOAA-17, launch June 24, 2002) the equator crossing time of the AM series spacecraft was changed from 7:30 AM to 10:00 AM (on descending node). Extreme Ultraviolet and X-ray Irradiance Sensors (EXIS)​. • NOAA-16 (L): The spacecraft, with a launch Sept. 21, 2000, is in backup mode for the PM orbit. 0.25 - Digital to analog - The digitally processed APT data are converted to a 2080 Hz bandwidth analog signal, amplitude modulated onto a 2.4 kHz carrier, and bandwidth limited to 4160 Hz in preparation for transmission by the VHF transmitters.

Click here for more information about GLM. AVHRR/3 provides some data processing provided by MIRP (Manipulated Information Rate Processor). The PTT capacity was increased from four to eight, this means eight DRU (Data Recovery Unit) on-board. The instrument's IFOV is 1.1º and the separation between the center of one Earth view to the next is 1.1º. 1988 is collected and processed across the Weather Enterprise and then fed to the AWIPS Program Network Control Facility which disseminates the products via the AWIPS Satellite Broadcast Network (SBN) / NOAAPort data broadcast via the Galaxy 28 Satellite. 36 On April 3, 2020, NOAA’s National Environmental Satellite, Data, and Information Service (NESDIS) began awarding contracts for satellite mission and instrument design analysis. NOAA-15 also collects data from buoys and remote weather stations for the ARGOS (Advanced Research and Global Observation Satellite) program dedicated to environmental study and protection. The sensor scans across-track in a `stop-and stare' mode (discrete stepping) at a scan rate of 6.4 s (56 Earth views per scan). ABI is the primary instrument on the GOES-R Series for imaging Earth’s weather, climate, oceans and the environment. LTAN (LTAN values are valid as of April 19, 2016), Table 5: Overview of POES operational missions, • May 20, 2015: Four MHS instruments are currently on orbit (on Metop-A and -B and NOAA-18 and -19) and are in good health — the only exception being one channel on NOAA-19. 5 2000, 0.37 OBCT (Onboard Calibration Target) is a hot target comprising an array of RF (Radio Frequency) absorbent pyramids. Channel 11 on the AMSU-A instrument failed in April 2002. A silicon photodiode at the instrument temperature (nominally 15º C) detects the visible energy. In addition to providing high-resolution atmospheric moisture profiles, AMSU-B is used to produce precipitation and surface products from two window channels. AMSU is a 20-channel microwave radiometer.

It is a zero-momentum system consisting of reaction wheels and Earth, sun, and inertial reference sensors. There are three types of direct broadcasting: (1) the real-time HRPT, (2) the direct sounder broadcast (DSB), also referred to as the real-time very high frequency (VHF) beacon transmissions, and (3) the Automatic Picture Transmission (APT). This was done to improve the utility of the data near cloud boundaries.

H Objectives: atmospheric temperature profile measurements from the surface up to about 50 km in 15 channels. This sensor is used on PM and late AM missions [NOAA-17 (-M) is in a 10 AM descending sun-synchronous orbit. Banks, "An overview of the NOAA/NESDIS data processing systems and derived products for NOAA-KLM," Earth System Monitor, Vol. 2 x 1000 (dual side band) These are key inputs for numerical weather prediction models, which are used operationally for weather forecasting worldwide. Central Pacific Hurricane Center 2525 Correa Rd Suite 250 Honolulu, HI 96822 W-HFO.webmaster@noaa.gov

Weather data (satellite imagery, radar data, model data, sensor data, etc.) The spacecraft structure has been stiffened primarily to support the heavier AMSU instruments and improve launch vehicle load margins. Each antenna provides a cross-track scan of ±48.33º from nadir with a total of 30 contiguous Earth views (stepped scan positions) per scan line. The Magnetometer provides measurements of the space environment magnetic field that controls charged particle dynamics in the outer region of the magnetosphere. The instrument is providing a humidity profiling capability in the frequency range of 89 - 190 GHz. John Bateman Each sensor consists of a dome of moderating material which absorbs energy from the particle (and so sets the detection energy threshold), a silicon solid state detector, a preamplifier, and a level comparator which responds to particles with enough energy to go through the moderator and produce a pulse from the detector large enough to exceed the level in the comparator. DCS-2: From NOAA-K onwards (satellites and its successors, there is a modified Argos data collection system referred to as DCS-2 (the predecessor of A-DCS). MHS technology used: advanced quasi-optics, planar millimetric frontends, precision calibration target, scan mechanism and reflector are combined with low power and mass electronics for minimum mass and power. 7 20) 21), TIR: <1.5% of 1.8º step size; SWIR: <1% of cha. Figure 3: Simplified block diagram of ADACS (image credit: NOAA), Sun-synchronous circular, altitude = 833±19 km or 870±19 km, inclination = 98.7º (retrograde), 4.18 m length, 1.88 m diameter, overall length = 7.4 m, 1479 kg on orbit, 2232 kg at launch (756 kg propellant), 833 W min, array size: 2.73 m x 6.14 m (16.76 m2), 5 DTR (Digital Tape Recorder), each with a capacity of 0.9 Gbit. NOAA POES Series - 5th Generation Satellites . Information provided by SEISS is used for assessing radiation hazards to astronauts and satellites and to warn of high flux events, mitigating damage to radio communications. Calibration of the IR channels is performed with four internal blackbodies every scan line.17) 18), 20.3 cm diameter afocal reflective Cassegrainian type, 21 cm x 29.5 cm elliptical ribbed beryllium, Two stage radiant cooler controlled @ 105 K, 40 kHz simultaneous sample of all channels, 200 k word/s max (2 Mbit/s in burst mode, 621.3 kbit/s average), Table 7: AVHRR/3 performance characteristics, Night cloud mapping, sea surface temperature, Table 8: Spectral parameters of AVHRR/3 channels, AVHRR/3 adds a sixth channel in the IR range at 1.61 µm (referred to as channel 3a, operating during the daylight part of the orbit). 0.84 The basic intent is to join the space segment of the emerging MetOp program of EUMETSAT with the existing POES program of NOAA into a fully coordinated service, thus sharing the costs of a program for synergetic reasons.

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