Names | AO-6 |
---|---|
Mission type | Amateur radio |
Operator | AMSAT / NASA |
COSPAR ID | 1972-082B |
SATCAT no. | 6236 |
Mission duration | 4.5 years (achieved) |
Spacecraft properties | |
Bus | AMSAT-OSCAR |
Manufacturer | AMSAT-NA |
Launch mass | 18.2 kg (40 lb) |
Dimensions | 16 cm × 30 cm × 44 cm (6.3 in × 11.8 in × 17.3 in) |
Power | 3.5 watts |
Start of mission | |
Launch date | 15 October 1972, 17:19 UTC |
Rocket | Delta 300 (Delta 91 / Thor 575575) |
Launch site | Vandenberg, SLC-2W |
Contractor | Douglas Aircraft Company |
End of mission | |
Last contact | 21 June 1977 |
Orbital parameters | |
Reference system | Geocentric orbit [1] |
Regime | Low Earth orbit |
Perigee altitude | 1,448 km (900 mi) |
Apogee altitude | 1,457 km (905 mi) |
Inclination | 101.70° |
Period | 114.93 minutes |
AMSAT-OSCAR 6 (a.k.a. AO-6) was the first Phase 2 amateur radio satellite (P2-A) launched into low Earth orbit. It was also the first satellite constructed by the new AMSAT North America (AMSAT-NA) organization.
The satellite was launched 15 October 1972, by a Delta 300 launcher from Vandenberg Air Force Base, Lompoc, California. AO-6 was launched piggyback with NOAA-2 (ITOS-D).
AMSAT-OSCAR 6 was box-shaped, measuring 43 cm × 30 cm × 15 cm, with a mass of 18.2 kg. It had a near-circular polar orbit of 1448 × 1457 km with an inclination of 101.70°. It deployed two quarter-wave monopole antennas, one each for 144 and 435 MHz, and half-wave dipole antenna for 29 MHz. It remained operational for 4.5 years until a battery failure on 21 June 1977. [2] [3]
Equipped with solar panels powering NiCd batteries, AO-6 provided 24 V at 3.5 watts power to three transponders. It carried a Mode A transponder (100 kHz wide at 1 watt) and provided store-and-forward morse and teletype messages (named Codestore) for later transmission. Subsystems were built in the United States, Australia, and Germany. [4]
AO-6 had a 1.3 watt transmitter into a half-wave dipole antenna. AO-6's receiver input sensitivity was approximately -100 dBm (2 μV per meter) and had an Automatic gain control (AGC) that provided up to 26 dB of gain reduction optimized for single-sideband modulation. The transceiver team consisted of Karl Meinzer DJ4ZC, Wallace Mercer W4RUD, Dick Daniels WA4DGU and Jan King W3GEY.
AO-6 demonstrated several uses of new technologies and operations. [4]
AMSAT is a name for amateur radio satellite organizations worldwide, but in particular the Radio Amateur Satellite Corporation (AMSAT) with headquarters at Washington, D.C. AMSAT organizations design, build, arrange launches for, and then operate (command) satellites carrying amateur radio payloads, including the OSCAR series of satellites. Other informally affiliated national organizations exist, such as AMSAT Germany (AMSAT-DL) and AMSAT Japan (JAMSAT).
AMSAT-OSCAR-40, also known as AO-40 or simply OSCAR 40, was the on-orbit designation of an amateur radio satellite of the OSCAR series. Prior to launch, the spacecraft was known as Phase 3D or "P3D". AO-40 was built by AMSAT.
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AMSAT-OSCAR 16, also known as AO-16 and PACSAT, is the in-orbit name designation of an amateur radio satellite of the OSCAR series. It was built by AMSAT and was launched on 22 January 1990 from Kourou, French Guiana on an Ariane 4 launch vehicle. It is in sun synchronous low Earth orbit.
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