NOAA-B

Last updated

NOAA-B
NamesNOAA-B
Mission type Weather
Operator NOAA
COSPAR ID 1980-043A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 11819
Mission duration2 years (planned)
339 days (achieved)
Spacecraft properties
Spacecraft typeTIROS
Bus TIROS-N [1]
Manufacturer RCA Astro Electronics [2]
Launch mass1,418 kg (3,126 lb) [3]
Dry mass735 kg (1,620 lb)
Start of mission
Launch date29 May 1980, 10:53:00 UTC [4]
Rocket Atlas F-Star-37S-ISS
(Atlas S/N 19F) [2]
Launch site Vandenberg, SLC-3W
Contractor Convair
End of mission
DisposalOrbital decay
Decay date3 May 1981 [4]
Orbital parameters
Reference system Geocentric orbit [4]
Regime Sun-synchronous orbit
Perigee altitude 273 km (170 mi)
Apogee altitude 1,453 km (903 mi)
Inclination 92.3°
Period 102.2 minutes
  NOAA-6
NOAA-7  
 

NOAA B was an American operational weather satellite for use in the National Operational Environmental Satellite System (NOESS) and for the support of the Global Atmospheric Research Program (GARP) during 1978-1984. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment. [5]

Contents

Launch

NOAA-B was launched by NASA on 29 May 1980 at 10:53 UTC. Intended for a Sun-synchronous orbit, the spacecraft entered a lower, elliptical orbit due to a launch vehicle malfunction resulting in a failed mission. Had the launch been successful it would have been designated NOAA-7. [6]

Following launch, a fuel leak between the turbopump and gearbox caused the main engine to lose 20–25% of its thrust. [7] [8] This caused the guidance system of the Atlas launch vehicle to increase the length of the first stage burn to compensate. [7]

Due to requirements specific to TIROS missions, there was no interface between the satellite and the launch vehicle guidance systems. [7] This resulted in the satellite attempting to separate from the launch vehicle at approximately 370 seconds after launch. The separation failed due to recontact between the Atlas - which was still under thrust - and the satellite, which only separated when the solid-fuel rocket motor intended to place NOAA-B into a circular 830 km (520 mi) Sun-synchronous orbit fired. [7]

Spacecraft

The satellite was based upon the DMSP Block 5D satellite bus developed for the U.S. Air Force, and it was capable of maintaining an Earth-pointing accuracy of better than ± 0.1° with a motion rate of less than 0.035 degrees/second. [5]

Instruments

Primary sensors included the Advanced Very High Resolution Radiometer (AVHRR/1) for global cloud cover observations, and the TIROS Operational Vertical Sounder (TOVS) suite for atmospheric temperature and water profiling. Secondary experiments consisted of a Space Environment Monitor (SEM) measuring proton and electron fluxes, and the Data Collection and Platform Location System (DCPLS) for relaying data from balloons and ocean buoys for the Argos system. The TOVS suite consists of three subsystems: the High Resolution Infrared Radiation Sounder 2 (HIRS/2), the Stratospheric Sounding Unit (SSU), and the Microwave Sounding Unit (MSU). [5]

Advanced Very High Resolution Radiometer

The NOAA 6 Advanced Very High Resolution Radiometer (AVHRR/1) was a four-channel scanning radiometer capable of providing global daytime and nighttime sea-surface temperature and information about ice, snow, and clouds. These data were obtained on a daily basis for use in weather analysis and forecasting. The multispectral radiometer operated in the scanning mode and measured emitted and reflected radiation in the following spectral intervals: channel 1 (visible), 0.55 to 0.90 micrometer (μm); channel 2 (near infrared), 0.725 μm to detector cutoff around 1.1 μm; channel 3 (IR window), 3.55 to 3.93 μm; and channel 4 (IR window), 10.5 to 11.5 μm. All four channels had a spatial resolution of 1.1 km, and the two IR-window channels had a thermal resolution of 0.12 Kelvin at 300 Kelvin. The AVHRR was capable of operating in both real-time or recorded modes. Real-time or direct readout data were transmitted to ground stations both at low (4 km) resolution via automatic picture transmission (APT) and at high (1 km) resolution via high-resolution picture transmission (HRPT). Data recorded on board were available for processing in the NOAA central computer facility. They included global area coverage (GAC) data, with a resolution of 4 km, and local area coverage (LAC), that contained data from selected portions of each orbit with a 1-km resolution. Identical experiments were flown on other spacecraft in the TIROS-N/NOAA series. [9]

TIROS Operational Vertical Sounder

The TIROS Operational Vertical Sounder (TOVS) consisted of three instruments: the High-resolution Infrared Radiation Sounder modification 2 (HIRS/2), the Stratospheric Sounding Unit (SSU), and the Microwave Sounding Unit (MSU). All three instruments were designed to determine radiances needed to calculate temperature and humidity profiles of the atmosphere from the surface to the stratosphere (approximately 1 mb). The HIRS/2 instrument had 20 channels in the following spectral intervals: channels 1 through 5, the 15-micrometer (μm) CO2 bands (15.0, 14.7, 14.5, 14.2, and 14.0 μm); channels 6 and 7, the 13.7- and 13.4-μm CO2/H2O bands; channel 8, the 11.1-μm window region; channel 9, the 9.7-μm ozone band; channels 10, 11, and 12, the 6-μm water vapor bands (8.3, 7.3, and 6.7 μm); channels 13 and 14, the 4.57- and 4.52-μm N2O bands; channels 15 and 16, the 4.46- and 4.40-μm CO2/N2O bands; channel 17, the 4.24-μm CO2 band; channels 18 and 19, the 4.0- and 3.7-μm window bands; and channel 20, the 0.70-μm visible region. The SSU instrument was provided by the British Meteorological Office (United Kingdom). It was similar to the Pressure-Modulated Radiometer (PMR) flown on Nimbus 6. The SSU operated at three 15.0-μm channels using selective absorption, passing the incoming radiation through three pressure-modulated cells containing CO2. The MSU instrument was similar to the Scanning Microwave Spectrometer (SCAMS) flown on Nimbus 6. The MSU had one channel in the 50.31-GHz window region and three channels in the 55-GHz oxygen band (53.73, 54.96, and 57.95 GHz) to obtain temperature profiles which were free of cloud interference. The HIRS/2 had a field of view (FOV) 30 km in diameter at nadir, whereas the MSU had a FOV of 110 km in diameter. The HIRS/2 sampled 56 FOVs in each scan line about 2250 km wide, and the MSU sampled 11 FOVs along the swath with the same width. Each SSU scan line had 8 FOVs with a width of 1500 km. This experiment was also flown on other TIROS-N/NOAA series spacecraft. [10]

Data Collection and Platform Location System

The Data Collection and Platform Location System (DCPLS) on NOAA-B, also known as Argos, was designed and built in France to meet the meteorological data needs of the United States and to support the Global Atmospheric Research Program (GARP). The system received low-duty-cycle transmissions of meteorological observations from free-floating balloons, ocean buoys, other satellites, and fixed ground-based sensor platforms distributed around the globe. These observations were organized on board the spacecraft and retransmitted when the spacecraft came within range of a Command and Data Acquisition (CDA) station. For free-moving balloons, the Doppler frequency shift of the transmitted signal was observed to calculate the location of the balloons. The DCPLS was expected, for a moving sensor platform, to have a location accuracy of 3 to 5 km, and a velocity accuracy of 1.0 to 1.6 m/s. This system had the capability of acquiring data from up to 4000 platforms per day. Identical experiments were flown on other spacecraft in the TIROS-N/NOAA series. Processing and dissemination of data were handled by CNES in Toulouse, France. [11]

Space Environment Monitor

The Space Environmental Monitor (SEM) was an extension of the solar proton monitoring experiment flown on the ITOS spacecraft series. The object was to measure proton flux, electron flux density, and energy spectrum in the upper atmosphere. The experiment package consisted of three detector systems and a data processing unit. The Medium Energy Proton and Electron Detector (MEPED) measured protons in five energy ranges from 30 keV to >2.5 MeV; electrons above 30, 100, and 300 keV; protons and electrons (inseparable) above 6 MeV; and omni-directional protons above 16, 36, and 80 MeV. The High-Energy Proton Alpha Telescope (HEPAT), which had a 48° viewing cone, viewed in the anti-Earth direction and measured protons in four energy ranges above 370 MeV and alpha particles in two energy ranges above 850 MeV/nucleon. The Total Energy Detector (TED) measured electrons and protons between 300 eV and 20 keV. [12]

Science objectives

Mission

Because the satellite had been unable to perform the pitch-down maneuver necessary to reach its intended orbit the spacecraft ended up in a highly elliptical orbit that was unsuitable for the intended mission. [6] [13] Following unsuccessful attempts to correct the orbit using the satellite's attitude control thrusters, NASA pronounced the mission a failure. [1] [6] [14]

Unlike the earlier Nimbus 1, which was also launched into an unplanned elliptical orbit following a launch vehicle malfunction, no attempt appears to have been made to operate the spacecraft instrumentation during its remaining lifetime in orbit. [5]

Related Research Articles

<span class="mw-page-title-main">Advanced microwave sounding unit</span> Instrument installed on meteorological satellites

The advanced microwave sounding unit (AMSU) is a multi-channel microwave radiometer installed on meteorological satellites. The instrument examines several bands of microwave radiation from the atmosphere to perform atmospheric sounding of temperature and moisture levels.

<span class="mw-page-title-main">Advanced very-high-resolution radiometer</span>

The Advanced Very-High-Resolution Radiometer (AVHRR) instrument is a space-borne sensor that measures the reflectance of the Earth in five spectral bands that are relatively wide by today's standards. AVHRR instruments are or have been carried by the National Oceanic and Atmospheric Administration (NOAA) family of polar orbiting platforms (POES) and European MetOp satellites. The instrument scans several channels; two are centered on the red (0.6 micrometres) and near-infrared (0.9 micrometres) regions, a third one is located around 3.5 micrometres, and another two the thermal radiation emitted by the planet, around 11 and 12 micrometres.

<span class="mw-page-title-main">NOAA-19</span> Weather satellite

NOAA-19, known as NOAA-N' before launch, is the last of the American National Oceanic and Atmospheric Administration (NOAA) series of weather satellites. NOAA-19 was launched on 6 February 2009. NOAA-19 is in an afternoon Sun-synchronous orbit and is intended to replace NOAA-18 as the prime afternoon spacecraft.

<span class="mw-page-title-main">NOAA-17</span>

NOAA-17, also known as NOAA-M before launch, was an operational, polar orbiting, weather satellite series operated by the National Environmental Satellite Service (NESS) of the National Oceanic and Atmospheric Administration (NOAA). NOAA-17 also continued the series of Advanced TIROS-N (ATN) spacecraft begun with the launch of NOAA-8 (NOAA-E) in 1983 but with additional new and improved instrumentation over the NOAA A-L series and a new launch vehicle.

<span class="mw-page-title-main">NOAA-16</span>

NOAA-16, also known as NOAA-L before launch, was an operational, polar orbiting, weather satellite series operated by the National Environmental Satellite Service (NESS) of the National Oceanic and Atmospheric Administration (NOAA). NOAA-16 continued the series of Advanced TIROS-N (ATN) spacecraft that began with the launch of NOAA-8 (NOAA-E) in 1983; but it had additional new and improved instrumentation over the NOAA A-K series and a new launch vehicle. It was launched on 21 September 2000 and, following an unknown anomaly, it was decommissioned on 9 June 2014. In November of 2015 it broke up in orbit, creating more than 200 pieces of debris.

<span class="mw-page-title-main">NOAA-18</span>

NOAA-18, also known as NOAA-N before launch, is an operational, polar orbiting, weather satellite series operated by the National Environmental Satellite Service (NESS) of the National Oceanic and Atmospheric Administration (NOAA). NOAA-18 also continued the series of Advanced TIROS-N (ATN) spacecraft begun with the launch of NOAA-8 (NOAA-E) in 1983 but with additional new and improved instrumentation over the NOAA A-M series and a new launch vehicle. NOAA-18 is in an afternoon equator-crossing orbit and replaced NOAA-17 as the prime afternoon spacecraft.

<span class="mw-page-title-main">NOAA-15</span> Longest Operating Weather Satellite

NOAA-15, also known as NOAA-K before launch, is an operational, polar-orbiting of the NASA-provided Television Infrared Observation Satellite (TIROS) series of weather forecasting satellite operated by National Oceanic and Atmospheric Administration (NOAA). NOAA-15 was the latest in the Advanced TIROS-N (ATN) series. It provided support to environmental monitoring by complementing the NOAA/NESS Geostationary Operational Environmental Satellite program (GOES).

NOAA-13, also known as NOAA-I before launch, was an American weather satellite operated by the National Oceanic and Atmospheric Administration (NOAA). NOAA-I continued the operational, polar orbiting, meteorological satellite series operated by the National Environmental Satellite System (NESS) of the National Oceanic and Atmospheric Administration (NOAA). NOAA-I continued the series (fifth) of Advanced TIROS-N (ATN) spacecraft begun with the launch of NOAA-8 (NOAA-E) in 1983. NOAA-I was in an afternoon equator-crossing orbit and was intended to replace the NOAA-11 (NOAA-H) as the prime afternoon (14:00) spacecraft.

<span class="mw-page-title-main">NOAA-7</span>

NOAA-7, known as NOAA-C before launch, was an American operational weather satellite for use in the National Operational Environmental Satellite System (NOESS) and for the support of the Global Atmospheric Research Program (GARP) during 1978-1984. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment. An earlier launch, NOAA-B, was scheduled to become NOAA-7, however NOAA-B failed to reach its required orbit.

NOAA-6, known as NOAA-A before launch, was an American operational weather satellite for use in the National Operational Environmental Satellite System (NOESS) and for the support of the Global Atmospheric Research Program (GARP) during 1978-1984. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment.

<span class="mw-page-title-main">Visible Infrared Imaging Radiometer Suite</span>

The Visible Infrared Imaging Radiometer Suite (VIIRS) is a sensor designed and manufactured by the Raytheon Company on board the polar-orbiting Suomi National Polar-orbiting Partnership, NOAA-20, and NOAA-21 weather satellites. VIIRS is one of five key instruments onboard Suomi NPP, launched on October 28, 2011. VIIRS is a whiskbroom scanner radiometer that collects imagery and radiometric measurements of the land, atmosphere, cryosphere, and oceans in the visible and infrared bands of the electromagnetic spectrum.

<span class="mw-page-title-main">NOAA-21</span> NASA/NOAA satellite

NOAA-21, designated JPSS-2 prior to launch, is the second of the United States National Oceanic and Atmospheric Administration (NOAA)'s latest generation of U.S. polar-orbiting, non-geosynchronous, environmental satellites called the Joint Polar Satellite System. NOAA-21 was launched on 10 November 2022 and join NOAA-20 and Suomi NPP in the same orbit. Circling the Earth from pole-to-pole, it will cross the equator about 14 times daily, providing full global coverage twice a day. It was launched with LOFTID.

<span class="mw-page-title-main">NOAA-20</span> NASA satellite

NOAA-20, designated JPSS-1 prior to launch, is the first of the United States National Oceanic and Atmospheric Administration's latest generation of U.S. polar-orbiting, non-geosynchronous, environmental satellites called the Joint Polar Satellite System. NOAA-20 was launched on 18 November 2017 and joined the Suomi National Polar-orbiting Partnership satellite in the same orbit. NOAA-20 operates about 50 minutes behind Suomi NPP, allowing important overlap in observational coverage. Circling the Earth from pole-to-pole, it crosses the equator about 14 times daily, providing full global coverage twice a day. This gives meteorologists information on "atmospheric temperature and moisture, clouds, sea-surface temperature, ocean color, sea ice cover, volcanic ash, and fire detection" so as to enhance weather forecasting including hurricane tracking, post-hurricane recovery by detailing storm damage and mapping of power outages.

<span class="mw-page-title-main">NOAA-5</span> Weather satellite operated by NOAA

NOAA-5, also known as ITOS-H was a weather satellite operated by the National Oceanic and Atmospheric Administration (NOAA). It was part of a series of satellites called ITOS, or improved TIROS, being the last of the series. NOAA-5 was launched on a Delta rocket on July 29, 1976.

<span class="mw-page-title-main">NOAA-8</span> Weather satellite

NOAA-8, known as NOAA-E before launch, was an American weather satellite operated by the National Oceanic and Atmospheric Administration (NOAA) for use in the National Environmental Satellite Data and Information Service (NESDIS). It was first of the Advanced TIROS-N series of satellites. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment.

<span class="mw-page-title-main">NOAA-9</span> American weather satellite

NOAA-9, known as NOAA-F before launch, was an American weather satellite operated by the National Oceanic and Atmospheric Administration (NOAA) for use in the National Environmental Satellite Data and Information Service (NESDIS). It was the second of the Advanced TIROS-N series of satellites. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment.

NOAA-10, known as NOAA-G before launch, was an American weather satellite operated by the National Oceanic and Atmospheric Administration (NOAA) for use in the National Environmental Satellite Data and Information Service (NESDIS). It was the third of the Advanced TIROS-N series of satellites. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment.

NOAA-11, known as NOAA-H before launch, was an American weather satellite operated by the National Oceanic and Atmospheric Administration (NOAA) for use in the National Operational Environmental Satellite System (NOESS) and for support of the Global Atmospheric Research Program (GARP) during 1978–1984. It was the fourth of the Advanced TIROS-N series of satellites. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment.

NOAA-12, also known as NOAA-D before launch, was an American weather satellite operated by National Oceanic and Atmospheric Administration (NOAA), an operational meteorological satellite for use in the National Environmental Satellite, Data, and Information Service (NESDIS). The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment.

NOAA-14, also known as NOAA-J before launch, was an American weather satellite operated by the National Oceanic and Atmospheric Administration (NOAA). NOAA-14 continued the third-generation operational, Polar Orbiting Environmental Satellite (POES) series operated by the National Environmental Satellite Service (NESS) of the National Oceanic and Atmospheric Administration (NOAA). NOAA-14 continued the series of Advanced TIROS-N (ATN) spacecraft begun with the launch of NOAA-8 (NOAA-E) in 1983.

References

  1. 1 2 "Tiros N". Encyclopedia Astronautica. Archived from the original on 28 December 2016. Retrieved 15 January 2017.
  2. 1 2 Krebs, Gunter. "TIROS-N, NOAA 6, B, 7". Gunter's Space Page. Retrieved 15 January 2017.
  3. "NOAA-6". World Meteorological Organisation (WMO). Retrieved 28 December 2020.
  4. 1 2 3 "Trajectory: NOAA-B 1980-043A". NASA. 14 May 2020. Retrieved 28 December 2020.PD-icon.svg This article incorporates text from this source, which is in the public domain.
  5. 1 2 3 4 "Display: NOAA-B 1980-043A". NASA GSFC. 14 May 2020. Retrieved 31 December 2020.PD-icon.svg This article incorporates text from this source, which is in the public domain .
  6. 1 2 3 "Satellite goes off its course". Spokane Daily Chronicle. 30 May 1980. p. 8. Retrieved 1 January 2013.
  7. 1 2 3 4 Eleazer, Wayne (31 December 2012). "Launch failures: engine out". The Space Review. Retrieved 1 January 2013.
  8. "Satellite in wrong orbit, a total loss". Merced Sun-Star. 30 May 1980. p. 27. Retrieved 1 January 2013.[ permanent dead link ]
  9. "AVHRR/1 1980-043A". NASA. 14 May 2020. Retrieved 31 December 2020.PD-icon.svg This article incorporates text from this source, which is in the public domain .
  10. "TOVS 1980-043A". NASA. 14 May 2020. Retrieved 31 December 2020.PD-icon.svg This article incorporates text from this source, which is in the public domain .
  11. "DCPLS 1980-043A". NASA. 14 May 2020. Retrieved 31 December 2020.PD-icon.svg This article incorporates text from this source, which is in the public domain .
  12. "SEM 1980-043A". NASA. 14 May 2020. Retrieved 31 December 2020.PD-icon.svg This article incorporates text from this source, which is in the public domain .
  13. "Weather Satellite Unstable". The Spokesman-Review. 30 May 1980. p. 14. Retrieved 1 January 2013.
  14. Bell, Peter M. (July 1980). "NOAA-B satellite mission unsuccessful". Eos . 61 (27): 515. Bibcode:1980EOSTr..61R.515B. doi:10.1029/EO061i027p00515-03.