Viking (satellite)

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Viking
Mission typeEarth observation
COSPAR ID1986-019B
SATCAT no.16614
Start of mission
Launch date22 February 1986 (1986-02-22)
RocketAriane 1
Launch siteGuiana Space Centre
Entered service22 February 1986
Orbital parameters
Reference systemGeocentric
RegimePolar
Semi-major axis13,550 km (8,420 mi)
Eccentricity0.0001538
Perigee801 km (498 mi)
Apogee13,538 km (8,412 mi)
Inclination98.7863°
Period261.56 minutes
Epoch15 April 2019, 18:22:45[1]
 
The Viking satellite is mounted on top of the Ariane adapter.

Viking was Sweden's first satellite. It was launched on an Ariane 1 rocket as a piggyback payload together with the French satellite SPOT 1, on February 22, 1986. Operations ended on May 12, 1987. Viking was used to explore plasma processes in the magnetosphere and the ionosphere.

Spacecraft[edit]

Space was limited underneath the SPOT 1 satellite, and Viking had to be quite sturdy in order to withstand the stress of launch. The basic shape of the Swedish satellite was a flat octagonal disc, 0.5 metres thick and 1.9 metres across. The mechanical interface of the payload adapter from the Ariane rocket was duplicated on top of Viking. This enabled it to be added to the launch with a minimum of redesign of the SPOT satellite. After SPOT had been released, Viking fired its own rocket engine and was sent into its proper polar orbit.

Mission[edit]

Once in orbit, 4 wire segments of 40 metre length each were spooled out in a radial direction from the edge of the spinning satellite disc. Also, 2 stiff rods of 4 metre length were extended in the axial direction. A sensor pod was stationed at the end of each of these, forming three orthogonal pairs. Together they could measure the electric field of the earth in all three dimensions. Stiff booms were also extended for other types of sensors and antennas.[citation needed]

The mission produced a large amount of extremely useful scientific data, and was deemed a great success. An initial discussion of what scientists learned from these measurements, which included "global distribution of magnetosphere-ionosphere interaction; auroral morphology and substorm dynamics; heating and expulsion of ionospheric plasma into the magnetosphere; field aligned acceleration into the ionosphere; and electron and ion wave generation"[2] can be found in the article "Scientific results from the Swedish Viking satellite", 1988 Swedish Inst. of Space Physics, Kiruna. Since then, many other scientific articles have been written using this important data set.[citation needed]

Post mission[edit]

After the scientific mission ended, both Viking and the upper stage of the rocket used to launch the satellite became derelict objects that would continue to orbit Earth for many years. As of September 2013, both objects remain in orbit.[3]

References[edit]

"VIKING - Sweden's first satellite". Swedish Space Corporation. Archived from the original on 2009-04-11. Retrieved 2008-11-18.[not specific enough to verify]

  1. ^ "Viking - Orbit". Heavens-Above. 15 April 2019. Retrieved 16 April 2019.
  2. ^ Scientific results from the Swedish Viking satellite Hultqvist, Bengt. Status Report, 1988 Swedish Inst. of Space Physics, Kiruna.
  3. ^ "Viking - Satellite Information". Satellite database. Heavens-Above. Retrieved 2013-09-21.

External links[edit]