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GOES 7

ResourceID
spase://SMWG/Observatory/GOES/7

Description

GOES 7 was the tenth in a series of NASA-developed, NOAA-operated, geosynchronous and
operational spacecraft. The spin-stabilized spacecraft carried (1) a visible infrared spin-scan
radiometer (VISSR) atmospheric sounder (VAS) to provide high-quality day/night cloudcover data,
to take radiance derived temperatures of the earth/atmosphere system, and to determine atmospheric
temperature and water vapor content at various levels, (2) a meteorological data collection system
to relay processed data from central weather facilities to regional stations equipped with APT and
to collect and retransmit data from remotely located earth-based platforms, and (3) a space
environment monitor (SEM) system to measure proton, electron, and solar X-ray fluxes and magnetic
fields. The cylindrically shaped spacecraft measured 190.5 cm in diameter and 230 cm in length,
exclusive of a magnetometer that extended an additional 83 cm beyond the cylindrical shell.
The primary structural members were a honeycombed equipment shelf and a thrust tube. The VISSR
telescope was mounted on the equipment shelf and viewed the earth through a special aperture in
the side of the spacecraft. A support structure extended radially from the thrust tube and was
affixed to the solar panels, which formed the outer wall of the spacecraft to provide the primary
source of electrical power. Located in the annulus-shaped space between the thrust tube and the
solar panels were stationkeeping and dynamics control equipment, batteries, and most of the SEM
equipment. Proper spacecraft attitude and spin rate (approximately 100 rpm) were maintained by
two separate sets of jet thrusters mounted around the spacecraft equator and activated by ground
command. The spacecraft used both UHF-band and S-band frequencies in its telemetry and command
subsystem. A low-power VHF transponder provided telemetry and command during launch and then
served as a backup for the primary subsystem once the spacecraft attains synchronous orbit.

  August 1999

  NASA's 12-year-old Geostationary Observational Environmental Satellite, GOES-7, is being

relocated to a position over the Pacific Ocean southwest of Hawaii to become part of PEACESAT,
the Pan Pacific Education and Communications Experiment by Satellite. More information on this
story can be found at:

  http://pao.gsfc.nasa.gov/gsfc/gnews/062599/062599.htm#goes7

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Details

Version:2.2.0

Observatory

ResourceID
spase://SMWG/Observatory/GOES/7
ResourceHeader
ResourceName
GOES 7
AlternateName
1987-022A
AlternateName
GOES-H
AlternateName
PEACESAT
ReleaseDate
2019-05-05 12:34:56Z
Description

GOES 7 was the tenth in a series of NASA-developed, NOAA-operated, geosynchronous and
operational spacecraft. The spin-stabilized spacecraft carried (1) a visible infrared spin-scan
radiometer (VISSR) atmospheric sounder (VAS) to provide high-quality day/night cloudcover data,
to take radiance derived temperatures of the earth/atmosphere system, and to determine atmospheric
temperature and water vapor content at various levels, (2) a meteorological data collection system
to relay processed data from central weather facilities to regional stations equipped with APT and
to collect and retransmit data from remotely located earth-based platforms, and (3) a space
environment monitor (SEM) system to measure proton, electron, and solar X-ray fluxes and magnetic
fields. The cylindrically shaped spacecraft measured 190.5 cm in diameter and 230 cm in length,
exclusive of a magnetometer that extended an additional 83 cm beyond the cylindrical shell.
The primary structural members were a honeycombed equipment shelf and a thrust tube. The VISSR
telescope was mounted on the equipment shelf and viewed the earth through a special aperture in
the side of the spacecraft. A support structure extended radially from the thrust tube and was
affixed to the solar panels, which formed the outer wall of the spacecraft to provide the primary
source of electrical power. Located in the annulus-shaped space between the thrust tube and the
solar panels were stationkeeping and dynamics control equipment, batteries, and most of the SEM
equipment. Proper spacecraft attitude and spin rate (approximately 100 rpm) were maintained by
two separate sets of jet thrusters mounted around the spacecraft equator and activated by ground
command. The spacecraft used both UHF-band and S-band frequencies in its telemetry and command
subsystem. A low-power VHF transponder provided telemetry and command during launch and then
served as a backup for the primary subsystem once the spacecraft attains synchronous orbit.

  August 1999

  NASA's 12-year-old Geostationary Observational Environmental Satellite, GOES-7, is being

relocated to a position over the Pacific Ocean southwest of Hawaii to become part of PEACESAT,
the Pan Pacific Education and Communications Experiment by Satellite. More information on this
story can be found at:

  http://pao.gsfc.nasa.gov/gsfc/gnews/062599/062599.htm#goes7
Contacts
RolePersonStartDateStopDateNote
1.ProjectScientistspase://SMWG/Person/William.E.Shenk
InformationURL
Name
NSSDC's Master Catalog
URL
Description

Information about the GOES 7 mission

InformationURL
Name
Earth Observation Resources Webpage on GOES
URL
Description

Detailed information about GOES Series.

PriorIDs
spase://SMWG/Observatory/GOES7
ObservatoryGroupID
Location
ObservatoryRegion
Earth.Magnetosphere.Main
OperatingSpan
StartDate
1987-02-26 00:00:00Z
StopDate
1996-08-13 08:30:00
Note
Useful operating span.