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

<https://gcmd.earthdata.nasa.gov/kms/concept/82b2d471-ddff-4c3c-8eed-82e834cc0029>
  ns0:altLabel [ ] ;
  skos:definition """Spacecraft Brief Description
  This  RAE-B  mission  was  the  second  of  a  pair of Radio Astronomy
  Explorer satellites.  It was placed into lunar orbit on June 15, 1973,
  to  provide  radio  astronomical measurements of the planets, the sun,
  and  the  galaxy  over the frequency range of 25 kHz to 13.1 MHz.  The
  experiment  complement consisted of two Ryle-Vonberg radiometers (nine
  channels  each),  three  swept-frequency  burst receivers (32 channels
  each),  and  an  impedance  probe  for  calibration.   The  experiment
  antennas  consisted  of  a 229-m upper V-antenna pointed away from the
  moon;  a  183-m  lower  V-antenna  pointed toward the moon; and a 37-m
  dipole antenna parallel to the lunar surface.  The lower V-antenna was
  extended  to  its  full 229-m length in November 1974.  The spacecraft
  body  was a truncated cylinder 36.25 in. in diameter and approximately
  31-in.  high,  with  four fixed solar paddles.  The maneuvering system
  consisted  of  a  hydrazine  velocity  correction  package, a cold gas
  attitude control system, and a solid fuel lunar insertion motor.  Data
  were  returned  to  the  earth  via  either  a low power UHF/(400 MHz)
  transmitter,  in  real time, or stored in an onboard tape recorder and
  transmitted  to  earth via a high power UHF transmitter (400 MHz). Two
  tape  recorders  provided  backup  storage.   A VHF transmitter served
  primarily  for  range  and  range-rate  measurements  and as a backup.
  Commands  were  received on a VHF (148 MHz) receiver, which also was a
  part  of  the  range  and  range-rate  system. Spacecraft attitude was
  determined  by (1) a solar aspect system, (2) a horizon sensor system,
  and (3) a panoramic attitude sensor system, and was accurate to 1 deg.
  The spacecraft was gravity gradient oriented (Z axis parallel to local
  vertical)  and  was  equipped  with  libration  dampers  to  damp  out
  oscillations.  For additional information, see J. K. Alexander et al.,
  Astron. & Astrophys., v. 40, p. 365, 1975.
Auxiliary Information
  Launch Date and Time : 1973-06-10 14:13:00
  Epoch Date and Time :  1973-06-21 00:00:00
  Orbit Type :  Geocentric
  Apogee(km) :  1063.84
  Perigee(km) : 1052.98
  Inclination :    55.7
  Date of last update :  1992-03-09
*** Note: For datasets information under this source name, select option 1
***       from the MD_MAIN menu, and then search by source."""@en ;
  skos:prefLabel "RAE-B"@en ;
  skos:inScheme <https://gcmd.earthdata.nasa.gov/kms/concepts/concept_scheme/platforms> ;
  skos:broader <https://gcmd.earthdata.nasa.gov/kms/concept/c381eef8-a0be-407e-b85b-67757d724af8> ;
  a skos:Concept .

<https://gcmd.earthdata.nasa.gov/kms/concept/c381eef8-a0be-407e-b85b-67757d724af8>
  skos:prefLabel "RAE (Radio Astronomy Explorer)"@en ;
  a skos:Concept ;
  skos:narrower <https://gcmd.earthdata.nasa.gov/kms/concept/82b2d471-ddff-4c3c-8eed-82e834cc0029> .

