@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/14b369b6-19d4-41fe-b1bc-27807ecb666d>
  skos:prefLabel "ATS (Advanced Technology Satellite)"@en ;
  a skos:Concept ;
  skos:narrower <https://gcmd.earthdata.nasa.gov/kms/concept/6988684a-7e7c-48a7-a1c3-2586dddd1fd4> .

<https://gcmd.earthdata.nasa.gov/kms/concept/6988684a-7e7c-48a7-a1c3-2586dddd1fd4>
  ns0:altLabel [ ] ;
  skos:definition """ATS 3 was launched in November 1967 and was one of a series of spacecraft
designed to demonstrate the utility and feasibility of a variety of
technological and scientific activities that could be carried out by an
earth-synchronous spacecraft.  Of the 11 experiments on board, 8 were
technological engineering experiments concerned with navigation,
communications, and spacecraft operation equipment; 2 were photographic imaging
experiments that produced near real-time daylight pictures of the
earth-atmosphere system; and the remaining experiment was an ionospheric
beacon.  The spin-stabilized spacecraft was cylindrically shaped and measured
180 cm in length and 142 cm in diameter.  The primary structural members were
a honeycombed equipment shelf and thrust tube.  Support rods extended radially
outward from the thrust tube and were affixed to solar panels which formed the
outer walls of the spacecraft.  Equipment components and payload were mounted
in the annular space between the thrust tube and solar panels.  In addition to
solar panels, the spacecraft was equipped with two rechargeable nickel-cadmium
batteries to provide electrical power.

This satellite supported an image dissector camera, multicolor spin scan
cloud cover camera, weather facsimile data relay system, omega position and
location equipment designed to demonstrate the feasibility of using the NAVY's
Omega Navigation System, and VHF, telemetry, and command antennas.  Spacecraft
guidance and orbital corrections were accomplished by 2.3 kg hydrogen peroxide
and hydrazine thrusters, which were activated by ground command.  Initially
placed at 48 degrees West over the Atlantic Ocean in a geosynchronous orbit,
the satellite position later varied between 45 and 95 degrees West in support
of meteorological operations.  In general, the various experiments were
successful.


Group: Platform_Details
   Entry_ID: ATS-3
   Group: Platform_Identification
      Platform_Category: Earth Observation Satellites
      Platform_Series_or_Entity: ATS (Advanced Technology Satellite)
      Short_Name: ATS-3
      Long_Name: Advanced Technology Satellite-3
   End_Group
   Group: Synonymous_Platform_Names
      Short_Name: Advanced Tech. Sat. 3
      Short_Name: 03029
   End_Group
   Creation_Date: 2007-08-29
   Online_Resource: http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=1967-111A
   Group: Platform_Logistics
      Launch_Date: 1967-11-05 
      Primary_Sponsor: NASA
   End_Group
End_Group"""@en ;
  skos:prefLabel "ATS-3"@en ;
  skos:inScheme <https://gcmd.earthdata.nasa.gov/kms/concepts/concept_scheme/platforms> ;
  skos:broader <https://gcmd.earthdata.nasa.gov/kms/concept/14b369b6-19d4-41fe-b1bc-27807ecb666d> ;
  a skos:Concept .

