@prefix skos: <http://www.w3.org/2004/02/skos/core#> .

<https://gcmd.earthdata.nasa.gov/kms/concept/95e65b17-0aa8-4146-999c-b807b42e8ad6>
  skos:definition """Venera 14 Mission Description:

Venera 13 and 14 were identical spacecraft built to take
advantage of the 1981 Venus launch opportunity and launched 5
days apart. The Venera 14 mission consisted of a bus (81-110A)
and an attached descent craft (81-110D). The Venera 14 descent
craft/lander was a hermetically sealed pressure vessel, which
contained most of the instrumentation and electronics, mounted
on a ring-shaped landing platform and topped by an antenna. The
design was similar to the earlier Venera 9-12 landers. It
carried instruments to take chemical and isotopic measurements,
monitor the spectrum of scattered sunlight, and record electric
discharges during its descent phase through the Venusian
atmosphere. The spacecraft utilized a camera system, an X-ray
fluorescence spectrometer, a screw drill and surface sampler, a
dynamic penetrometer, and a seismometer to conduct
investigations on the surface.  After launch and a four month
cruise to Venus, the descent vehicle separated from the bus and
plunged into the Venus atmosphere on 5 March 1982. After
entering the atmosphere a parachute was deployed. At an altitude
of about 50 km the parachute was released and simple airbraking
was used the rest of the way to the surface. Venera 14 landed
about 950 km southwest of Venera 13 near the eastern flank of
Phoebe Regio at 13 deg 15 min S by 310 E on a basaltic
plain. After landing an imaging panorama was started and a
mechanical drilling arm reached to the surface and obtained a
sample, which was deposited in a hermetically sealed chamber,
maintained at 30 degrees C and a pressure of about .05
atmospheres. The composition of the sample was determined by the
X-ray flourescence spectrometer, showing it to be similar to
oceanic tholeiitic basalts. The lander survived for 57 minutes
(the planned design life was 32 minutes) in an environment with
a temperature of 465 degrees C and a pr!  essure of 94 Earth
atmospheres. The descent vehicle transmitted data to the bus,
which acted as a data relay as it.

[Source: NASA]


Group: Platform_Details
   Entry_ID: VENERA-14
   Group: Platform_Identification
      Platform_Category: Interplanetary Spacecraft
      Platform_Series_or_Entity: LANDER
      Short_Name: VENERA-14
   End_Group
   Online_Resource: http://heasarc.gsfc.nasa.gov/docs/heasarc/missions/venera1314.html
End_Group"""@en ;
  skos:prefLabel "VENERA-14"@en ;
  skos:inScheme <https://gcmd.earthdata.nasa.gov/kms/concepts/concept_scheme/platforms> ;
  skos:broader <https://gcmd.earthdata.nasa.gov/kms/concept/c12d28c9-5a4c-4897-b82b-67ed59d14e75> ;
  a skos:Concept .

<https://gcmd.earthdata.nasa.gov/kms/concept/c12d28c9-5a4c-4897-b82b-67ed59d14e75>
  skos:prefLabel "LANDER"@en ;
  a skos:Concept ;
  skos:narrower <https://gcmd.earthdata.nasa.gov/kms/concept/95e65b17-0aa8-4146-999c-b807b42e8ad6> .

