The Alouette 1 satellite
|Harvard designation||1962 Beta Alpha 1|
|Launch mass||145.6 kilograms (321 lb) |
|Start of mission|
|Launch date||29 September 1962, 06:05UTC|
|Rocket||Thor DM-21 Agena-B|
|Launch site||Vandenberg LC-75-1-1|
|End of mission|
|Semi-major axis||7,381.48 kilometres (4,586.64 mi)|
|Perigee||992 kilometres (616 mi)|
|Apogee||1,027 kilometres (638 mi)|
|Epoch||4 December 2013, 19:55:17 UTC|
Alouette 1 is a deactivated Canadian satellite that studied the ionosphere. Launched in 1962, it was Canada's first satellite, and the first satellite constructed by a country other than the USSR or the United States. Canada was the fourth country to operate a satellite, as the British Ariel 1, constructed in the United States by NASA, preceded Alouette 1 by five months.
The purpose of Alouette 1 was to investigate the properties of the top of the ionosphere, and the dependence of those properties on geographical location, season, and time of day. Alouette 1 was advanced for its time, and NASA initially doubted whether the available technology would be sufficient. Nevertheless, NASA were eager to collaborate with international partners. NASA were convinced to participate by the prospect of obtaining data on the ionosphere, and Canada had the additional objective of developing their own space research programme.
Satellite launch and mission progress
Alouette 1 was launched by NASA from the Pacific Missile Range at Vandenberg Air Force Base, California, USA at 06:05 UTC on September 29, 1962, into orbit around the earth. It was placed into an almost circular orbit of altitude 987 kilometres (613 mi) to 1,022 kilometres (635 mi) with an inclination of 80.5°. The launch made Canada the third nation, after the USSR and the United States, to design and construct its own satellite. Alouette was used to study the ionosphere, an area of the upper atmosphere where many future satellites would be placed into orbit, using over 700 different radio frequencies to investigate its properties from above.
The satellite was initially spin-stabilised, rotating 1.4 times per minute. After about 500 days, the rotation had slowed to about 0.6 rpm and the spin-stabilisation failed at this point. It was then only possible to determine the satellite's orientation by readings from a magnetometer and from temperature sensors on the upper and lower heat shields. The orientation determinations obtained this way were only accurate to within 10 degrees. It is likely that gravitational gradients had caused the longest antenna to point towards the Earth.
Alouette 's mission lasted for 10 years before the satellite was deliberately switched off. The mission brought a modicum of fame to its Program Manager, John E. Jackson, Canadian director, John Herbert Chapman and its Chief Electrical Engineer, Colin Franklin.[clarification needed]
Alouette 1 remains in orbit and in 1966 it was estimated that Alouette 1 would remain in orbit for 1000 years.
Two satellites were built for redundancy in case of a malfunction; if the first unit failed, the second could be launched with only a couple of months delay. It took 3½ years after Alouette 's proposal to have it developed and built. The satellites S27-2 (prototype), S27-3 (which became the launched satellite), and S27-4 (which became the backup) were assembled by Defence Research Telecommunications Establishment (DRTE) Electronics Lab in Ottawa. The mechanical frame and the deployable STEM antennas were made by the Special Products and Applied Research (SPAR) division of de Havilland Canada (DHC) in Downsview, Ontario, in a building which many years later (until 2012) housed the Canadian Air and Space Museum. The batteries used for Alouette were developed by the Defence Chemical, Biological, and Radiation Laboratory (DCBRL), another branch of DRB, and were partially responsible for the long lifetime of the satellite. The "Storable Tubular Extendable Member" antennas used were the first of DHC's STEM antennas used in space, and at launch were the longest (125 feet tip to tip). When completed Alouette weighed 145 kg (320 lb) and was launched from a Thor-Agena-B two-stage rocket. Alouette 1 's backup was later launched as Alouette 2 in 1965 to "replace" the older Alouette 1.
Alouette 1 carried four scientific experiments:
- Sweep-Frequency Sounder. This experiment measured the electron density distribution in the ionosphere by measuring the time delay between the emission and return of radio pulses. The sounder was able to emit pulses with frequencies between 1 and 12 megahertz, with a power of 100W.
- Energetic particle detectors. An arrangement of Geiger counters and scintillators for detecting energetic particles.
- VLF Receiver. An experiment for measuring both artificial and natural VLF signals. It was sensitive to frequencies between 400 and 10,000 Hz.
- Cosmic Radio Noise. Two long radio antennas for detecting radio noise from the Sun and the Galaxy.
After Alouette 1 was launched, the upper stage of the rocket used to launch the satellite became a derelict object that would continue to orbit Earth for many years. As of September 2013[update], the upper stage remains in orbit.
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