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Observatory

ResourceID
spase://SMWG/Observatory/GOES/4
ResourceHeader
ResourceName
Geostationary Operational Environmental Satellites 4
AlternateName
GOES 4
AlternateName
1980-074A
ReleaseDate
2019-05-05 12:34:56Z
Description

GOES 4 was the sixth in a series of NASA-developed, NOAA-operated, geosynchronous and
operational spacecraft. The spin-stabilized spacecraft carried (1) a VISSR (visible infrared spin
scan radiometer) 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 and
transmission system to relay processed data from central weather facilities to APT-equipped
regional stations 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 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 walls 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 had
attained synchronous orbit. When GOES 5 VAS experienced a failure on July 30, 1984, GOES 4 was
reactivated by NOAA to provide GOES 1 VISSR data relay services to western users.

Acknowledgement
NASA; Mr. Adolph J. Cervenka; Mr. Gerald W. Longanecker; Mr. William E. Shenk
Contacts
RolePersonStartDateStopDateNote
1.ProjectScientistspase://SMWG/Person/William.E.Shenk
2.MetadataContactspase://SMWG/Person/James.M.Weygand
InformationURL
Name
NSSDC's Master Catalog on GOES 4
URL
Description

Information about the GOES 4 mission

InformationURL
Name
Earth Observation Resources Webpage on GOES
URL
Description

Detailed information about GOES Series.

PriorIDs
spase://SMWG/Observatory/GOES4
ObservatoryGroupID
Location
ObservatoryRegion
Earth.Magnetosphere.RadiationBelt
ObservatoryRegion
Earth.NearSurface.Plasmasphere
ObservatoryRegion
Earth.Magnetosphere.Main
CoordinateSystemName
GSM
OperatingSpan
StartDate
1980-09-09 00:00:00Z
StopDate
1982-11-26 23:59:59
Note
Useful operating span.