Advanced Research and Global Observation Satellite

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ARGOS
Type: Experimental satellite
Country: United StatesUnited States United States
Operator: US Air Force
COSPAR-ID : 1999-008A
Mission dates
Dimensions: 2720 ​​kg
Begin: February 23, 1999, 10:29 UTC
Starting place: Vandenberg SLC-2
Launcher: Delta-7920-10 D267
Flight duration: 3 years
Status: Automatically switched off
Orbit data
Rotation time : 102 min
Orbit inclination : 98.7 °
Apogee height 842 km
Perigee height 822 km

The Advanced Research and Global Observation Satellite , ARGOS for short , was an American experimental satellite that carried out scientific experiments from 1999 to 2002.

Furnishing

The satellite was equipped with the following devices:

  • High-temperature super-conductive experiment II (HTSSE)
  • Extreme Ultraviolet Photometer (EUVIP)
  • Electric propeller room test (ESEX)
  • Unconventional Stellar Aspect (USA)
  • Space dust (SPADUS)
  • Critical Ionization Velocity (CIV)
  • High resolution airglow / aurora spectroscope (HIRAAS)
  • Global Ionosphere Imaging Monitor (GIMI)

The energy was supplied by two fold-out solar modules and batteries.

The contract for the development and manufacture of the satellite was awarded to the Space Systems Division of Rockwell International in Seal Beach . This area was later taken over by Boeing.

Mission history

ARGOS was launched on February 23, 1999 in a Delta 7920-10 launcher from Vandenberg Air Force Base SLC-2 .

It was automatically turned off about three years after it started.

Web links

Individual evidence

  1. Original orbit data according to ARGOS in the NSSDCA Master Catalog , accessed on April 28, 2017 (English).
  2. Harold W. Ennulat: Paper Session III-B - The Advanced Research and Global Observation Satellite (ARGOS) - Pioneering Advancements in Space. (PDF) In: The Space Congress Proceedings. Paper April 25, 1996, pp. 8-17 , accessed July 9, 2017 .
  3. ^ John Mintz: Boeing To Buy Rockwell's Defense, Space Division. Washington Post, August 2, 1996, accessed July 9, 2017 .