Names | BE-C Beacon Explorer-C Beacon-C NASA S-66C |
---|---|
Mission type | Ionospheric research |
Operator | NASA |
COSPAR ID | 1965-032A |
SATCAT no. | 01328 |
Mission duration | 59 years, 6 months and 29 days (in orbit) |
Spacecraft properties | |
Spacecraft | Explorer XXVII |
Bus | Beacon Explorer |
Manufacturer | Johns Hopkins University Applied Physics Laboratory |
Launch mass | 60.8 kg (134 lb) |
Dimensions | 30 × 45 cm (12 × 18 in) |
Power | 4 deployable solar arrays and batteries |
Start of mission | |
Launch date | 29 April 1965, 14:17:00 GMT |
Rocket | Scout X-4 (S-136R) |
Launch site | Wallops Flight Facility, |
Contractor | Vought |
Entered service | 29 April 1965 |
End of mission | |
Last contact | 20 July 1973 |
Orbital parameters | |
Reference system | Geocentric orbit[1] |
Regime | Low Earth orbit |
Perigee altitude | 927 km (576 mi) |
Apogee altitude | 1,320 km (820 mi) |
Inclination | 41.10° |
Period | 107.70 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]