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Equator-S
The Equator-S satellite was operational between 2 December 1997 and 1 May 1998 [1]
Mission type Heliophysics
Operator ISTP
COSPAR ID 1997-075B Edit this at Wikidata
SATCAT no.25068 Edit this on Wikidata
Website https://www2011.mpe.mpg.de/EQS/eq-s-home.html
Mission duration150 days [1]
Spacecraft properties
Manufacturer Max Planck Institute for Extraterrestrial Physics [1]
Launch mass230 kg (510 lb) [2]
Start of mission
Launch date2 December 1997
End of mission
Last contact1 May 1998
 

The Equator-S satellite was a spacecraft constructed by the Max Planck Institute for Extraterrestrial Physics for the International Solar-Terrestrial Physics Science Initiative. It was operational between 2 December 1997 and 1 May 1998. [1]

Computer generated image of the Equator-S satellite (NASA).

Description

Equator-S was a low-cost mission, launched with the intention to study the Earth's magnetosphere around the equator at heights lower than 67,000 km. [1] It was located in a near-equatorial orbit, which gave Equator-S the ability to make unique observations about the interaction between the magnetosphere and interplanetary space. [3] Equator-S had a very high spin rate and was launched on an Ariane 4 rocket on 2 December 1997. [1]

The mission ended earlier than expected, having initially been intended to have a lifetime of two years. The mission was terminated on 1 May 1998 after the failure of the onboard processor system. [1]

See also

References

  1. ^ a b c d e f g "Max Planck Institute- Equator S Summary". Retrieved 9 December 2021.
  2. ^ "Spacecraft Specs". MP:EquatorS Archive. Max Planck Institute. Retrieved 9 December 2021.
  3. ^ "NASA: Equator-S". NASA. Retrieved 13 December 2021.
From Wikipedia, the free encyclopedia

Equator-S
The Equator-S satellite was operational between 2 December 1997 and 1 May 1998 [1]
Mission type Heliophysics
Operator ISTP
COSPAR ID 1997-075B Edit this at Wikidata
SATCAT no.25068 Edit this on Wikidata
Website https://www2011.mpe.mpg.de/EQS/eq-s-home.html
Mission duration150 days [1]
Spacecraft properties
Manufacturer Max Planck Institute for Extraterrestrial Physics [1]
Launch mass230 kg (510 lb) [2]
Start of mission
Launch date2 December 1997
End of mission
Last contact1 May 1998
 

The Equator-S satellite was a spacecraft constructed by the Max Planck Institute for Extraterrestrial Physics for the International Solar-Terrestrial Physics Science Initiative. It was operational between 2 December 1997 and 1 May 1998. [1]

Computer generated image of the Equator-S satellite (NASA).

Description

Equator-S was a low-cost mission, launched with the intention to study the Earth's magnetosphere around the equator at heights lower than 67,000 km. [1] It was located in a near-equatorial orbit, which gave Equator-S the ability to make unique observations about the interaction between the magnetosphere and interplanetary space. [3] Equator-S had a very high spin rate and was launched on an Ariane 4 rocket on 2 December 1997. [1]

The mission ended earlier than expected, having initially been intended to have a lifetime of two years. The mission was terminated on 1 May 1998 after the failure of the onboard processor system. [1]

See also

References

  1. ^ a b c d e f g "Max Planck Institute- Equator S Summary". Retrieved 9 December 2021.
  2. ^ "Spacecraft Specs". MP:EquatorS Archive. Max Planck Institute. Retrieved 9 December 2021.
  3. ^ "NASA: Equator-S". NASA. Retrieved 13 December 2021.

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