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AMSAT-OSCAR 6

AMSAT-OSCAR 6
Mission type Amateur radio
COSPAR ID 1972-082B
SATCAT no. 6236
Spacecraft properties
Launch mass 18.2 kilograms (40 lb)
Start of mission
Launch date 15 October 1972 (1972-10-15)
Rocket Delta 300
Launch site Vandenberg SLC-2W
End of mission
Last contact 21 June 1977 (1977-06-22)
Orbital parameters
Reference system Geocentric
Regime Low Earth
Perigee 1,448 kilometres (900 mi)
Apogee 1,457 kilometres (905 mi)
Inclination 101.7 degrees
Period 114.93 minutes
Epoch 15 November 1972

AO-6 (a.k.a. AMSAT-OSCAR 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 October 15, 1972 by a Delta 300 launcher from Vandenberg Air Force Base, Lompoc, California. AO-6 was launched piggyback with ITOS-D (NOAA 2).

Weight 18.2 kg. Orbit 1450 x 1459 km. Inclination 101.7 degrees. Box shaped 430 x 300 x 150 mm. Quarter-wave monopole antennas (144 and 435 MHz) and half-wave dipole antenna (29 MHz). It remained operational for 4.5 years until a battery failure on June 21, 1977.

Equipped with solar panels powering NiCd batteries, AO-6 provided 24 V at 3.5 W power to three transponders. It carried a Mode A transponder (100 kHz wide at 1 W) and provided store-and-forward morse and teletype messages (named Codestore) for later transmission. Subsystems were built in the United States, Australia, and Germany.

AO-6 had a 1.3 watt transmitter into a half-wave dipole antenna. AO-6's receiver input sensitivity was approximately -100dbm (2 uv per meter) and had an AGC that provided up to 26 dB of gain reduction optimized for SSB 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.

 This article incorporates public domain material from websites or documents of the National Aeronautics and Space Administration.


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