GOES-16

Instrument conceptualization The Geostationary Operational Environmental Satellite (GOES) program began as a joint effort between the National Aeronautics and Space Administration (NASA) and the National Oceanic and Atmospheric Administration (NOAA) in 1975 to develop geostationary weather satellites following the success of the Applications Technology Satellite (ATS) and Synchronous Meteorological Satellite programs beginning in 1966. In the 1999 Operational Requirements Document (ORD) for the Evolution of Future NOAA Operational Geostationary Satellites, NOAA listed instrument requirements for the next generation of GOES imager and sounder. Top priorities included continuous observation capabilities, the ability to observe weather phenomena at all spatial scales, and improved spatial and temporal resolution for both the imager and sounder. These specifications laid the conceptual foundations for the instruments that would eventually be included with GOES-16. More concrete development of GOES-16 began with the initial designs of an Advanced Baseline Imager (ABI), which started in June 1999 under the direction of Tim Schmitt of the National Environmental Satellite, Data, and Information Service (NESDIS). At its inception, ten spectral bands were considered for inclusion in the new ABI, derived from six instruments on other satellites. In September 1999, the NOAA Research and Development Council endorsed the continued development of the instrument with the suggested bandwidths and frequencies. As the instrument became further realized, the number of potential spectral bands increased from the initial ten, to twelve by October 1999. Initial forecasts were for the ABI to be included as part of GOES beginning with the projected launch of GOES-Q in 2008. In 2001, NOAA planned for the GOES-R generation of GOES satellites to commence with the expected launch of GOES-R in 2012, with the ABI and ABS as expected instrumentation. GOES-R and its sister satellites were to lead to substantial improvements in forecast accuracy and detail by providing new operational products for users. Four years later, the number of proposed spectral bands on the ABI instrument increased to 16, covering a swath of visible and infrared wavelengths. In September 2006, NOAA dropped plans to include the HES aboard GOES-R, citing a lack of sufficient testing and major cost overruns in the development of the National Polar-orbiting Operational Environmental Satellite System (NPOESS). Although the GOES-R series was expected to cost in total, increased instrument complexity, revised inflation assumptions, and program reserves led to the Government Accountability Office estimating a much higher US$11.4 billion cost for the program in 2006. Construction In December 2008, NASA and NOAA selected Lockheed Martin Space Systems as the contractor for the fabrication of the first two satellites of the GOES-R generation, including GOES-R, for an estimated value of contract at US$1.09 billion. Preliminary design review was completed just over two years later, with critical design review being completed in May 2012. Construction of the satellite bus was contracted out to Alliant Techsystems (ATK) and work began shortly thereafter, with the core structure becoming test-ready in January 2013. The Extreme Ultraviolet and X-ray Irradiance Sensors (EXIS) became the first installation-ready instruments for GOES-R in May 2013, while the ABI became integration-ready in February 2014; spacecraft propulsion and system modules were delivered three months later, finalizing the initial construction phase and allowing for complete spacecraft integration and testing at Lockheed Martin's facilities in Colorado. The satellite was then transferred to Kennedy Space Center on 22 August 2016 to undergo additional tests and ready the spacecraft for launch. ==Spacecraft design==

GOES-16 and other satellites of the GOES-R generation are based around a derivative of Lockheed Martin's A2100 spacecraft bus capable of supporting up to dry mass with power capabilities exceeding 4 kW until the spacecraft's end-of-life. GOES-16 is powered by a solar array containing five solar panels that were folded at launch and unfurled after deployment. GOES-16 was designed to have a service lifetime of 15 years, including 10 years as an operational satellite and 5 additional years as a backup for successive GOES satellites. GOES-16's command and data handling subsystem is based around the SpaceWire bus; a modified version of the SpaceWire protocol was developed specifically for GOES-16 as a cost and risk reduction measure, with the associated application-specific integrated circuit being developed by British Aerospace. The GOES Reliable Data Delivery Protocol (GRDDP) complements preexisting SpaceWire capabilities and includes packet loss detection and recovery. ==Instruments==

Earth-facing The Advanced Baseline Imager (ABI) and Geostationary Lightning Mapper (GLM) make up GOES-16's Earth-facing, or nadir-pointing, instruments. These are positioned on a stable precision-pointed platform isolated from the rest of the spacecraft. all electronics and the sensor array are redundant to ensure operation longetivity. Several other companies were involved in the development and fabrication of the ABI, including BAE Systems, BEI Technologies, Babcock Corporation, DRS Technologies, L3 Technologies SSG-Tinsley, and Northrop Grumman Space Technology. The ABI takes images with three different geographic extents, In the default "flex" mode (scan mode 3) of operation, the ABI produces full-disk images of the Earth every 15 minutes, with a spatial resolution of . The instrument also images a area centered on the continental United States every five minutes at a resolution of . Where possible, the ABI can also image mesoscale phenomena over two selected areas every 60 seconds at a resolution of . The ABI onboard GOES-16 represents a significant improvement over the imager onboard previous GOES satellites. The sixteen spectral bands on the ABI, as opposed to the five on the previous GOES generation, represents a two-fold increase in spectral information. In addition, the ABI features up to four times greater spatial resolution and five times greater temporal resolution over the previous GOES imager. The ABI is nearly identical to the Advanced Himawari Imager (AHI) first used on the Japan Meteorological Agency's Himawari 8, which launched on 7 October 2014. The two instruments share 15 of the same spectral bands and have one spectral band unique to either instrument, with the ABI featuring a 1.37 μm near-infrared band for cirrus cloud detection while the AHI uses a 0.51 μm band optimized for reflectance around the green portion of the visible spectrum. Lacking an explicit band for green light, true-color imagery for ABI is created using the combination of the ABI's red and blue visible bands along with a synthesized green band; the simulated green band is created by applying algorithms based on MODIS and AHI onto existing ABI spectral bands. Geostationary Lightning Mapper (GLM) The GOES-16 Geostationary Lightning Mapper (GLM) is a single-channel near-infrared detector that monitors for the short-lived light emitted by lightning. by extension, such information can also reduce false alarm rates of severe thunderstorm and tornado warnings. The GLM can detect both cloud-to-cloud and cloud-to-ground lightning during daytime and nighttime, complementing land-based lightning detection. GLM's sensitivity results in a detection rate of 70–90% of all lightning strikes in its viewing area. The camera is a 1372 × 1300 pixel staring CCD sensitive to 777.4 nm light with a spatial resolution of at the nadir and near the edge of the instrument's field-of-view, resulting in a spatial resolution averaging roughly . The latitudinal coverage of the instrument is limited to between 52°N and 52°S. To limit interference of undesired light, a solar blocking filter and solar rejection filter are affixed to the front of the instrument's aperture. Data from the GLM can be mapped in real-time using open-source software that has also been adapted by the United States National Weather Service Development of the GLM was contracted by the Lockheed Martin Advanced Technology Center in Palo Alto, California. Sun-facing The Sun-facing, or solar-pointing, components of GOES-16 include the EXIS and SUVI, which are located on a Sun Pointing Platform (SPP) on the spacecraft's solar array yoke; the SPP tracks the seasonal and daily movement of the sun relative to GOES-16, and also supports GOES-16's Unique Payload Services. Together, the EXIS instrument weighs and consumes 40 W of power. Solar Ultraviolet Imager (SUVI) The Solar Ultraviolet Imager (SUVI) is an ultraviolet telescope onboard GOES-16 that produces full-disk images of the sun in the extreme ultraviolet range, succeeding the former GOES Solar X-ray Imager instrument onboard previous GOES satellite generations. The goals of SUVI are to locate coronal holes, detect and locate solar flares, monitor changes that indicate coronal mass ejections, detect active regions beyond the Sun's east limb, and analyze the complexity of active regions on the sun. The telescope is composed of six different wavelength bands centered between 94–304 Å specialized for different solar features. The GOES-16's ultraviolet imager is analogous to the Extreme ultraviolet Imaging Telescope on the Solar and Heliospheric Observatory. Space environment GOES-16 features two instruments, the Magnetometer (MAG) and Space Environment In-Situ Suite (SEISS), that provide localized in-situ observations of high-energy particles and magnetic fields in geostationary orbit. Magnetometer (MAG) The GOES-16 Magnetometer (MAG) is a tri-axial fluxgate magnetometer that measures the Earth's magnetic field at the outer extents of the magnetosphere from geostationary orbit. MAG provides general data on geomagnetic activity, which can be used to detect solar storms and validate large-scale space environment modelling; The magnetometer samples the magnetic field at a resolution of 0.016 nT at a frequency of 2.5 Hz. The electronic and sensor components of MAG were built by Macintyre Electronic Design Associates, Inc. (MEDA) in Sterling, Virginia, while the deployable boom was built by ATK in Goleta, California. Space Environment In-Situ Suite (SEISS) The Space Environment In-Situ Suite (SEISS) consists of four sensors with a wide variance in field-of-view that monitor proton, electron, and heavy ion fluxes in the magnetosphere. Electrons at these energies easily penetrate spacecraft and may cause internal dielectric breakdown or discharge damage. Development of SEISS was contracted by Assurance Technology Corporation in Carlisle, Massachusetts, and subcontracted to the University of New Hampshire. ==Launch and mission profile==

NASA selected the Atlas V 541 operated by United Launch Services as the launch vehicle for GOES-R on 5 April 2012, with a launch date slated for October 2015 from Cape Canaveral Air Force Station Space Launch Complex 41. Combined with the subsequent GOES-S, launch operations were expected to cost US$446 million. The launch date was chosen relatively early to maintain the operation of the GOES satellite constellation despite there being only a 48% confidence in meeting the October 2015 launch date; an audit by the Office of Inspector General of the Department of Commerce in April 2013 highlighted these concerns and projected a February 2016 launch which would reduce development stress at the cost of increasing the risk for gaps in satellite coverage should the operational backup satellites fail. Difficulties with GOES-R software and communications equipment caused the expected launch to be delayed to early 2016, and on 15 October 2015, the launch was pushed further to 13 October 2016. In early October 2016, GOES-R was secured in preparation for the close passage of Hurricane Matthew and did not sustain any damage. However, the tipping of a ground system rail van housing the spacecraft and the discovery of a booster fault on the Atlas V rocket—the same issue that had prevented the launch of WorldView-4 earlier in 2016—resulted in another delay of the launch window to 19 November 2016. On 18 November 2016, the mated GOES-R spacecraft and the Atlas V launch vehicle were moved to the launch pad at Space Launch Complex 41. GOES-R was launched on 19 November 2016 at 23:42 UTC (6:42 p.m. EST) from Cape Canaveral Air Force Station Space Launch Complex 41 aboard an Atlas V rocket. An undisclosed issue on the Eastern Range and verification of a potential concern on another rocket had delayed the launch by an hour towards the end of the 19 November launch window. The Atlas V's ascent was directed slightly south of east over the Atlantic Ocean. Following the rocket's first stage, additional burns in subsequent stages steered the spacecraft towards the altitude needed for geosynchronous orbit. Spacecraft separation from the launch vehicle occurred over Indonesia roughly 3.5 hours after launch, placing GOES-R in an elliptical low-inclination geostationary transfer orbit with a perigee of and an apogee of . During the first corrective burn, the truss holding the main engine nozzle warmed to anomalously high temperatures. Although the exceeded pre-flight temperature limits were revised, the subsequent four burns were limited to less than 41 minutes each in duration out of an abundance of caution, bringing it to its preliminary geostationary orbit ten days after launch. In reaching geostationary orbit, GOES-R was redesignated as GOES-16, beginning a yearlong extended checkout and validation phase. The spacecraft was initially positioned in a non-operational test position at 89.5°W, with GOES-13 and GOES-15 serving as the operational weather satellites in the traditional GOES East and GOES West positions, respectively. while the first images from ABI were collected on 15 January 2017 and released on 23 January 2017. On 25 May 2017, NOAA announced that GOES-16 would occupy the GOES East position once operational, succeeding GOES-13. GOES-16's move to its operational position began at around 13:30 UTC on 30 November 2017, drifting about 1.41° per day to a final longitude of 75.2°W; during this time, the spacecraft's instruments were kept in a diagnostic mode without data collection or transmission. GOES-16 reached the GOES East position by 11 December, and following a calibration period, resumed instrument data collection and transmission three days later. On 18 December 2017, GOES-16 was declared fully operational. ==Unique Payload Services and data processing==

Unique Payload Services In addition to its primary science payload, GOES-16 also features the Unique Payload Services (UPS) suite which provide communications relay services ancillary to the mission's primary operations: • GOES Rebroadcast (GRB) – GOES-16's downlink is handled by the GRB system, which serves as the primary full resolution and near-real-time relay for the satellite's instrument data. The instrument data are processed as Level 1b data for all instruments and Level 2 data for the GLM. The GRB replaces the former GOES VARiable (GVAR) service used by previous GOES spacecraft. The dual circular polarized signal is centered within the L band at 1686.6 MHz and consists of two 15.5 Mbit/s digital streams for a total data rate of 31 Mbit/s. • Data Collection System (DCS) – GOES-16 also serves as a relay satellite that rebroadcasts in-situ ground environmental observations, typically from remote locations, to other ground receiving sites. The GOES-16 DCS supports 433 user-platform channels with a downlink frequency range of 1679.70–1680.10 MHz. • Emergency Managers Weather Information Network (EMWIN) – EMWIN transmits products and other information from the United States National Weather Service. EMWIN is also coupled with the High Rate Information Transmission (HRIT) service, which broadcasts low-resolution GOES imagery and selected products to remotely located user HRIT terminals. The antennas at Wallops are designed to withstand sustained winds of and gusts of up to , conditions expected in a Category 2 hurricane. In 2009, NOAA contracted the Government Communications Systems Division of Harris Corporation with the development of the GOES-R ground system, with an estimated value of contract at US$736 million; Harris was also awarded a US$130 million contract to develop the ground antenna system, including six new large-aperture transceiving antennas and upgrades to four existing antennas at the NOAA Satellite Operations Facility. To aid in systems engineering and data distribution tools for the ground segment, Boeing was awarded a $55 million subcontract. In addition to GRB, which can be accessed by any calibrated receiver, GOES data is also distributed through other channels. The National Weather Service receives data directly from GOES-16 through the Advanced Weather Interactive Processing System (AWIPS) interface, which integrates meteorological and hydrological data with the agency's forecast and warning issuance systems. Real-time GOES-16 data is available through the Product Distribution and Access (PDA) system, while archived data is stored on the Comprehensive Large Array-data Stewardship System (CLASS). The technological proving ground addressed recommendations from the National Research Council in 2000 for NOAA to develop teams demonstrating the scope of new sensors like those on GOES-16 in concert with instrument design. The AWIPS-centric program was designed to allow for evaluation and development of simulated GOES-R products and provide training for forecasters. Participants in the proving ground program were classified as developers—those developing the satellite algorithms and training materials for GOES-R products—or users—the recipients of those products. The three primary developers in the program were the Cooperative Institute for Meteorological Satellite Studies (CIMSS) and Advanced Satellite Products Branch (ASPB) at the University of Wisconsin in Madison, Wisconsin; the Cooperative Institute for Research in the Atmosphere (CIRA) and Regional and Mesoscale Meteorology Branch (RAMMB) at Colorado State University in Fort Collins, CO; and NASA's Short-term Prediction Research and Transition Center (NASA SPoRT) in Huntsville, Alabama. severe storm development, aviation, and air quality. ==See also==