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Alouette 1

ResourceID
spase://SMWG/Observatory/Alouette1

Description

Alouette 1 was a small ionospheric observatory instrumented with an ionospheric sounder, a VLF receiver,
an energetic particle detector, and a cosmic noise experiment. Extended from the satellite shell were two dipole
antennas (45.7 m and 22.8 m long, respectively) which were shared by three of the experiments on the spacecraft.
The satellite was spin-stabilized at about 1.4 rpm after antenna extension. After about 500 days, the spin slowed more
than had been expected, to about 0.6 rpm when satellite spin-stabilization failed. It is believed that the satellite
gradually progressed toward a gravity gradient stabilization with the longer antenna pointing earthward. Attitude
information was deduced only from a single magnetometer and temperature measurements on the upper and lower heat shields.
Attitude determination could have been in error by as much as 10 degrees. There was no tape recorder, so data were available
only from the vicinity of telemetry stations. Telemetry stations were located to provide primary data coverage near the 80
degree W meridian and in areas near Hawaii, Singapore, Australia, Europe, and Central Africa. Initially, data were recorded
for about six hours per day. In September 1972, spacecraft operations were terminated. A data restoration effort began in the
late nineties and successfully saved a considerable portion of the high-resolution data before the telemetry tapes were
discarded.

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Details

Version:2.2.0

Observatory

ResourceID
spase://SMWG/Observatory/Alouette1
ResourceHeader
ResourceName
Alouette 1
AlternateName
1962-049A
AlternateName
Alouette-A
ReleaseDate
2019-05-05 12:34:56Z
Description

Alouette 1 was a small ionospheric observatory instrumented with an ionospheric sounder, a VLF receiver,
an energetic particle detector, and a cosmic noise experiment. Extended from the satellite shell were two dipole
antennas (45.7 m and 22.8 m long, respectively) which were shared by three of the experiments on the spacecraft.
The satellite was spin-stabilized at about 1.4 rpm after antenna extension. After about 500 days, the spin slowed more
than had been expected, to about 0.6 rpm when satellite spin-stabilization failed. It is believed that the satellite
gradually progressed toward a gravity gradient stabilization with the longer antenna pointing earthward. Attitude
information was deduced only from a single magnetometer and temperature measurements on the upper and lower heat shields.
Attitude determination could have been in error by as much as 10 degrees. There was no tape recorder, so data were available
only from the vicinity of telemetry stations. Telemetry stations were located to provide primary data coverage near the 80
degree W meridian and in areas near Hawaii, Singapore, Australia, Europe, and Central Africa. Initially, data were recorded
for about six hours per day. In September 1972, spacecraft operations were terminated. A data restoration effort began in the
late nineties and successfully saved a considerable portion of the high-resolution data before the telemetry tapes were
discarded.

Contacts
RolePersonStartDateStopDateNote
1.ProjectScientistspase://SMWG/Person/John.E.Jackson
InformationURL
Name
NSSDC's Master Catalog
URL
Description

Information about the Alouette 1 mission

Location
ObservatoryRegion
Earth.Magnetosphere