Superbird-A1
Superbird-A1, also identified as Superbird-1A before launch, was a geostationary communications satellite designed and manufactured by Ford Aerospace on the SSL 1300 platform. It was originally ordered by Space Communications Corporation, which later merged into the SKY Perfect JSAT Group. It had a mixed Ku band and Ka band payload and operated on the 158°E longitude.
It was ordered in 1985 along Superbird-B, Superbird-A1 and Superbird-B1 on the very first order of the SSL 1300 platform.Satellite description
The spacecraft was the fourth satellite designed and manufactured by Ford Aerospace on the SSL 1300 satellite bus. It was based on the design of the Intelsat V series and offered a three-axis stabilized platform.
It had a launch mass of and a 10-year design life. When stowed for launch, its dimensions were. With its solar panels fully extended it spanned. Its power system generated approximately 3,984 W of power due to two wings with three solar panels each. It also a NiH2 battery to survive the solar eclipses. It would serve as the main satellite on the 158°E longitude position of the Superbird.
Its propulsion system included an R-4D-11 LAE with a thrust of. It included enough propellant for orbit circularization and 10 years of operation.
Its payload is composed of 14 Ku band plus 30 Ka band transponders.History
Space Communications Corporation was founded in 1985, the same year as the original companies that later formed JSAT. On 1986 SCC ordered four spacecrafts, Superbird-1, Superbird-2, Superbird-A1 and Superbird-B1 from Ford Aerospace, which became Space Systems/Loral on October 1990.
On December 1, 1992 at 22:37:18 UTC Superbird-A1, was launched aboard an Ariane 42P. It was injected into a 192 km × 35,990 km × 7° geosynchronous transfer orbit, from which it climbed through three liquid apogee engine firings. It was positioned in its 158°East longitude position where it was integrated to the Superbird-A communication network.
