The "SACI" satellites are composed of a multi-mission platform and a set of experiments that constitute the payload. These satellites had the cooperation of several Brazilian and foreign institutions.
The SACI-1 scientific satellite has the following characteristics:
Format: parallelepiped with 60 cm x 40 cm x 40 cm
Mass: 60 kg
Orbit: heliosynchronous
Stabilization: by rotation (6 rpm)
Precision: 1 degree
Energy supply
Solar Cells: Gallium Arsenide (AsGa)
Dimensions: 3 panels of 57 x 44 cm
Efficiency: 19%
Power output: 150W
Nickel Cadmium (NiCd) Battery Cells
Voltage: 1.4 V
Capacity: 4.5 Ah
Remote control rate: 19.2 kbit/s
Transmission rate: 500 kbit/s
Antennas of edge: 2 of transmission and 2 of reception, type Microstrip
Although the launch went smoothly, and the intended orbit reached, SACI-1 did not come into operation, probably due to a failure in the solar panel control system.
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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