Explorer 27

Explorer 27
Depiction of Explorer 27 in orbit
NamesBE-C
Beacon Explorer-C
Beacon-C
NASA S-66C
Mission typeIonospheric research
OperatorNASA
COSPAR ID1965-032A Edit this at Wikidata
SATCAT no.01328
Mission duration59 years, 6 months and 20 days
(in orbit)
Spacecraft properties
SpacecraftExplorer XXVII
BusBeacon Explorer
ManufacturerJohns Hopkins University
Applied Physics Laboratory
Launch mass60.8 kg (134 lb)
Dimensions30 × 45 cm (12 × 18 in)
Power4 deployable solar arrays and batteries
Start of mission
Launch date29 April 1965, 14:17:00 GMT
RocketScout X-4 (S-136R)
Launch siteWallops Flight Facility,
ContractorVought
Entered service29 April 1965
End of mission
Last contact20 July 1973
Orbital parameters
Reference systemGeocentric orbit[1]
RegimeLow Earth orbit
Perigee altitude927 km (576 mi)
Apogee altitude1,320 km (820 mi)
Inclination41.10°
Period107.70 minutes
Instruments
Langmuir probes
Laser Tracking Reflectors
Radio Beacon
Radio Doppler System
Explorer program

Explorer 27 (or BE-C or Beacon Explorer-C, Beacon-C or S-66C) was a small NASA satellite, launched in 1965, designed to conduct scientific research in the ionosphere.[2] It was powered by 4 solar panels. One goal of the mission was to study in detail the shape of the Earth by way of investigating variations in its gravitational field.[3] It was the third and last of the Beacons in the Explorers program. The satellite was shut off in July 1973 so that its transmission band could be used by higher-priority spacecraft.[2]

  1. ^ "Trajectory: Explorer 27 (BE-C) 1965-032A". NASA. 28 October 2021. Retrieved 8 November 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  2. ^ a b "Display: Explorer 27 (BE-C) 1965-032A". NASA. 28 October 2021. Retrieved 8 November 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  3. ^ "Explorer Series of Spacecraft". NASA. Retrieved 12 April 2018.