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]