@prefix skos: <http://www.w3.org/2004/02/skos/core#> .
@prefix ns0: <http://gcmd.gsfc.nasa.gov/kms#> .

<https://gcmd.earthdata.nasa.gov/kms/concept/f91ad0ef-29bd-4594-a843-60beaaf858ca>
  skos:prefLabel "NIMBUS"@en ;
  a skos:Concept ;
  skos:narrower <https://gcmd.earthdata.nasa.gov/kms/concept/6b956645-9c85-4b3d-8771-159a62005911> .

<https://gcmd.earthdata.nasa.gov/kms/concept/6b956645-9c85-4b3d-8771-159a62005911>
  ns0:resource [ ] ;
  skos:changeNote """2015-05-12 12:54:13.0 [saritz]  
update PrefLabel (Nimbus-4); 
""", """2019-03-26 17:35:02.0 [sritz]  
update Resource (image); 
insert WeightedRelation (id: null
related concept uuid: 7bf9f69e-3bc7-45ad-9224-969676d36d78
relationship type: null
relationship value: null
generated by: null); 
""", """2019-03-26 17:35:45.0 [sritz]  
update WeightedRelation (Platform-Instrument); 
update WeightedRelation (1); 
""" ;
  skos:definition """Nimbus-4 was launched in April 1970 and was the fourth in a series of
second-generation meteorological research-and-development satellites that was
designed to serve as a stabilized, earth-oriented platform for the testing of
advanced meteorological sensor systems and for collecting meteorological data.
The polar-orbiting spacecraft consisted of three major structures: (1) a
ring-shaped sensor mount, (2) solar paddles, and (3) the control system
housing. The solar paddles and the control system were connected to the sensor
mount by a truss structure, giving the satellite the appearance of an ocean
buoy. Nimbus-4 was nearly 3.7 m tall, 1.45 m in diameter at the base, and about
3 m across with solar paddles extended. The torus-shaped sensor mount, which
formed the satellite base, housed the electronics equipment and battery
modules. The lower surface of the torus ring provided mounting space for
sensors and telemetry antennas. An H-frame structure mounted within the center
of the torus provided support for the larger experiments and tape recorders.
Mounted on the control system housing, which was on top of the spacecraft, were
sun sensors, horizon scanners, gas nozzles for attitude control, and a command
antenna. Use of an advanced attitude-control subsystem permitted the
spacecraft's orientation to be controlled to within plus or minus 1 degree for
all three axes (pitch, roll, and yaw).
Primary experiments consisted of an image dissector camera system for providing
daytime cloudcover pictures both in real-time and recorded modes,
temperature-humidity infrared radiometer (THIR) for measuring daytime and
nighttime surface and cloudtop temperatures as well as the water vapor content
of the upper atmosphere, infrared interferometer spectrometer (IRIS) for
measuring the emission spectra of the earth/atmosphere system, satellite
infrared spectrometer (SIRS) for determining the vertical profiles of
temperature and water vapor in the atmosphere, a monitor of ultraviolet solar
energy (MUSE) for detecting solar UV radiation, a backscatter ultraviolet (BUV)
detector for monitoring the vertical distribution and total amount of
atmospheric ozone on a global scale, a filter wedge spectrometer (FWS) for
accurate measurement of IR radiance as a function of wavelength from the
earth/atmosphere system, a selective chopper radiometer (SCR) for determining
the temperatures of six successive 10-km layers in the atmosphere from
absorption measurements in the 15-micrometer CO2 band, and an interrogation,
recording, and location system (IRLS) for locating, interrogating, recording,
and retransmitting meteorological and geophysical data from remote collection
stations. The spacecraft performed well until April 14, 1971, when attitude
problems started. The experiments then operated on a limited time basis until
September 30, 1980.
__________
Taken from the NSSDC System for Information Retrieval and Storage (SIRS).  For
more information contact the NSSDC Coordinated Request and User Support Office,
301-286-6695 (NASA Goddard Space Flight Center, Code 933.4, Greenbelt, Maryland
20771, USA).
Nimbus-4 User's Guide.


Group: Platform_Details
   Entry_ID: NIMBUS-4
   Group: Platform_Identification
      Platform_Category: Earth Observation Satellites
      Platform_Series_or_Entity: NIMBUS
      Short_Name: NIMBUS-4
   End_Group
   Group: Synonymous_Platform_Names
      Short_Name: NIMBUS-D
   End_Group
   Group: Platform_Associated_Instruments
      Short_Name: NEAR-INFRARED SPECTROMETER
      Short_Name: BUV
   End_Group
   Creation_Date: 2007-10-11
   Online_Resource: http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=1970-025A
   Online_Resource: http://nasascience.nasa.gov/missions/nimbus
   Sample_Image: http://space.skyrocket.de/img_sat/nimbus-4__1.jpg
   Group: Platform_Logistics
      Launch_Date: 1970-04-08
      Launch_Site: Vandenberg Air Force Base, USA
      Primary_Sponsor: USA/NASA
   End_Group
End_Group"""@en ;
  skos:prefLabel "Nimbus-4"@en ;
  skos:inScheme <https://gcmd.earthdata.nasa.gov/kms/concepts/concept_scheme/platforms> ;
  skos:broader <https://gcmd.earthdata.nasa.gov/kms/concept/f91ad0ef-29bd-4594-a843-60beaaf858ca> ;
  a skos:Concept .

