Superbird-A1
{{Use American English|date=March 2021}}
{{Use dmy dates|date=March 2021}}
{{Infobox spaceflight
| name = Superbird-A1
| names_list = Superbird-1A
| image =
| image_caption =
| image_size = 300px
| mission_type = Communications
| operator = Space Systems/Loral
| SATCAT = 22253
| website =
| mission_duration = 10 years (planned)
| spacecraft = Superbird-A1
| spacecraft_type = Superbird
| spacecraft_bus = SSL 1300
| manufacturer = Ford Aerospace
| launch_mass = {{cvt|2780|kg}}
| dry_mass =
| dimensions = Stowed: {{cvt|2.41|x|2.58|x|2.20|m}}
Solar panels extended: {{cvt|20.3|m}}
| power = 4 kW
| launch_date = 1 December 1992, 22:48:00 UTC
| launch_rocket = Ariane-42P H10+
| launch_site = Cebtre Spatial Guyanais, ELA-2
| launch_contractor = Arianespace
| entered_service =
| disposal_type =
| deactivated =
| last_contact =
| orbit_reference = Geocentric orbit
| orbit_regime = Geostationary orbit
| orbit_longitude = 158° East
| apsis = gee
| trans_band = 14 Ku-band
30 Ka-band
| trans_frequency =
| trans_bandwidth =
| trans_capacity =
| trans_coverage = Japan
| insignia =
| insignia_caption =
| insignia_size = 200px
| programme = Superbird constellation
| previous_mission = Superbird-B1
| next_mission = Superbird-C
}}
Superbird-A1, also identified as Superbird-1A before launch, was a geostationary communications satellite designed and manufactured by Ford Aerospace (now Space Systems/Loral) on the SSL 1300 satellite bus. It was originally ordered by Space Communications Corporation (SCC), which later merged into the SKY Perfect JSAT Group. It had a mixed Ku-band and Ka-band payload and operated on the 158° East 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 {{cvt|2780|kg}} and a 10-year design life. When stowed for launch, its dimensions were {{cvt|2.41|x|2.58|x|2.20|m}}. With its solar panels fully extended it spanned {{cvt|20.3|m}}. Its power system generated approximately 4 kW 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 liquid apogee engine (LAE) with a thrust of {{cvt|490|N}}. 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 (SCC) was founded in 1985, the same year as the original companies that later formed JSAT. On 1986 SCC ordered four spacecraft, Superbird-1, Superbird-2, Superbird-A1 and Superbird-B1 from Ford Aerospace, which became Space Systems/Loral in October 1990.
On 1 December 1992 at 22:48:00 UTC Superbird-A1, was launched aboard an Ariane 42P. It was injected into a 192 km × 35,990 km × 7° geosynchronous transfer orbit (GTO), from which it climbed through three liquid apogee engine (LEA) firings. It was positioned in its 158° East longitude position where it was integrated to the Superbird communication network.
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References
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{{Orbital launches in 1992}}
Category:Communications satellites in geostationary orbit
Category:Satellites using the SSL 1300 bus
Category:Spacecraft launched in 1992