Dove-OSCAR 17

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Dove-OSCAR 17
File:OSCAR-17 (DOVE) Promotion Photo.jpg
a.k.a Microsat 2
Mission type Educational, Amateur radio
Operator Brazil BRAMSAT
Spacecraft properties
Launch mass 12.92 kilograms (28.5 lb)
Power Solar panels and batteries
Start of mission
Launch date 22 January 1990 (1990-01-22)
Rocket European Union Ariane 4
Launch site French Guiana Kourou, French Guiana
End of mission
Last contact March 1998 (1998-04)
Orbital parameters
Reference system Sun-synchronous
Regime Low Earth
Perigee 791 km (492 mi)
Apogee 821 km (510 mi)
Inclination 98.7 degrees
Period 100.8 minutes

Dove-OSCAR 17 (aka DO-17 or Microsat 2) is a Brazilian educational and amateur radio satellite launched at January 22, 1990.

Project

Dove-OSCAR 17 is one the results of the so called Microsat project by AMSAT, manufactured in the 1980s by the civil and electric engineer Junior Torres de Castro (amateur radio operator with callsign PY2BJO), who had been developing his ideas since 1957. He has built, with his own resources, the first artificial satellite for educational and humanitarian purposes: the "Dove".

The device, assembled in a garage in São Paulo, was meant to provide synthesised peace messages for educational institutions at a time when the Cold War was still determining international relations around the world. It has a Digital Orbiting Voice Encoder (D.O.V.E.), designed to emit the synthesised voice messages, and also telemetry data transmission (FM Packet AFSK 1200 AX.25 at 145.825 MHz). It is box shaped with dimensions of 213 × 230 × 230 mm, with solar panels on the faces of the cube and weights 12.92 kg.[1] The configuration and assembly was at that time designated as "Microsat".[2]

Mission

Dove-OSCAR 17 was launched at January 22, 1990 by an Ariane 4 rocket from Guiana Space Center. The payload also included the SPOT-2 and other five OSCAR satellites. According to AMSAT, "due to hardware failures that have occurred since launch, the primary mission of providing voice messages of world peace from DOVE has not been fully realized"[3]

Last stable contact with the satellite officially occurred in March 1998 when it had a battery failure. However, because of the still functional solar panels, when the device is properly aligned to the Sun, it transmits its telemetry data.

See also

References

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External links