The spacecraft was designed and manufactured by then Hughes Space and Communications Company (now Boeing Satellite Development Center) on the HS-601 satellite bus. It had a launch mass of 3,150kg (6,940lb), a dry mass of 1,416kg (3,122lb) and a 13-year design life. When stowed for launch, it measured 4m ×3.8m ×2.4m (13.1ft ×12.5ft ×7.9ft). It had two wings with four solar panels each, that generated 4.5 kW at the end of its design life. When fully deployed, the solar panels spanned 26.2m (86ft), with its antennas in fully extended configuration it was 7.5m (25ft) wide.[6][7] It had a 29-cell NiH2 battery with a power charge of 200 Ah.[7]
Its payload is composed of two 2.2m (7ft 3in) dual-gridded reflectors and twenty four Ku-bandtransponders powered by a traveling-wave-tube amplifier (TWTA) with and output power of 90 watts. It can configure two 54MHz transponders into one 114MHz with an effective 180 watts.[6][7]
The Ku-band footprint covered Japan, southern and eastern Asia, and Hawaii.[7]
History
Space Communications Corporation (SCC) was founded in 1985, the same year as the original companies that later formed JSAT.[8] SCC switched satellite suppliers and on 1995 ordered a satellite from Boeing, Superbird-C.[6]
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets).