Generated by DeepSeek V3.2| OSCAR 13 | |
|---|---|
| Name | OSCAR 13 |
| Mission type | Amateur radio communications |
| Operator | AMSAT |
| COSPAR ID | 1988-051B |
| SATCAT | 19270 |
| Launch date | 15 June 1988 |
| Launch rocket | Ariane 3 |
| Launch site | Guiana Space Centre |
| Mission duration | 8 years (achieved) |
| Spacecraft bus | AMSAT Phase III |
| Power | Solar panels |
OSCAR 13. OSCAR 13 was a highly advanced Amateur radio satellite developed and operated by the international AMSAT organization. Launched in 1988, it represented a major leap in capability as part of the Phase III series, providing long-duration, worldwide communications for radio amateurs. Its sophisticated design and extended operational life made it one of the most successful and beloved satellites in amateur radio history.
OSCAR 13 was the fourth successful satellite in the AMSAT Phase III program, following the pioneering missions of AMSAT-OSCAR 10. Its primary purpose was to facilitate non-commercial two-way communication and experimentation across continents using VHF, UHF, and microwave bands. The spacecraft served as a transponder in a high Molniya orbit, allowing for extended communication passes over the Northern Hemisphere. This mission cemented the critical role of volunteer-built technology in advancing Space technology and global DX communication.
The satellite was based on a modular, octagonal spacecraft bus, a design refined from earlier AMSAT projects like AMSAT-OSCAR 10. Its structure was stabilized using a sophisticated spin-stabilization system and a patented yo-yo de-spin mechanism. For power, it relied on body-mounted gallium arsenide solar cells, which charged nickel-cadmium batteries. The core communications payload included a linear transponder with receivers on 145 MHz and 435 MHz, and transmitters on 435 MHz and 2.4 GHz, enabling modes like SSB and CW.
OSCAR 13 was launched as a secondary payload on 15 June 1988 aboard an Ariane 3 rocket from the Guiana Space Centre in French Guiana. Its primary companion on the launch was the Meteosat P2 weather satellite for the European Space Agency. The launch vehicle successfully injected OSCAR 13 into a targeted transfer orbit, after which the satellite's own solid-fuel Apogee kick motor fired to place it into its operational Molniya orbit. This high-inclination, elliptical orbit with a 12-hour period provided optimal coverage for North America, Europe, and Asia.
Following initial checkout and deployment of its antennas, OSCAR 13 entered full service in July 1988. It immediately became a cornerstone of the global Amateur radio community, reliably supporting countless contacts, including school group demonstrations and emergency communications drills. The satellite far exceeded its designed lifespan, operating nominally for eight years despite gradual degradation of its batteries. Its mission was officially declared ended in 1996 after the failure of its attitude control system, which prevented further usable operation of its transponders.
For radio amateurs worldwide, accessing OSCAR 13 required equipment capable of tracking its rapidly moving orbit and handling the Doppler shift on its UHF and Microwave links. Operators used Yagi antennas and specialized transceivers or software-defined radios to communicate through its transponders. The satellite enabled pioneering work in EME-style weak-signal communication and was instrumental in awards like the AMSAT Satellite Communications Achievement Award. Its legacy is preserved by subsequent satellites like AMSAT-OSCAR 40 and the Fox series of cubesats. Category:Amateur radio satellites Category:Spacecraft launched in 1988 Category:AMSAT