Manufacturer | INVAP |
---|---|
Country of origin | Argentina |
Operator | ARSAT S.A. |
Applications | Communications |
Specifications | |
Spacecraft type | Geostationary Communications satellite |
Launch mass | 2,900 kg (6,400 lb) to 3,000 kg (6,600 lb) |
Dry mass | < 1,500 kg (3,300 lb) |
Payload capacity | 350 kg (770 lb) and 3.5 kW[1] |
Dimensions | Bus without payload nor solar panels:2 m (6.6 ft) × 1.8 m (5.9 ft) × 2.9 m (9.5 ft) Span with solar panels deployed: (16.5 m (54 ft) |
Power | 4.2 kW (end of life) |
Equipment | Ku band, Ka band and C Band payloads. |
Regime | Geostationary |
Design life | 15 years |
Production | |
Status | In Production |
On order | 3 |
Built | 2 |
Launched | 2 |
Operational | 1 |
Maiden launch | 16 October 2014, 21:43ARSAT-1 | UTC,
ARSAT-3K is a geostationary communications satellite bus designed and manufactured by INVAP of Argentina for the local telecommunication company ARSAT S.A.[2][3] It is a small (4.2 kW of power generation and 3,000 kg (6,600 lb) of launch mass) three axis stabilized platform designed, manufactured and tested completely in Argentina.[4][5] It is capable of carrying up to 350 kg (770 lb) of payload with a maximum power consumption of 3.4 kW at the end of life. It currently[when?] uses only chemical propulsion, but a hybrid solution which would use bi-propellant propulsion for orbit raising and electric propulsion for station keeping is being developed. A purely electric propulsion version is planned.[6]
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