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Firewheel (Feuerrad)

Firewheel (with 4 Subsats on top) [MPE]

The Firewheel spacecraft was designed to make barium and lithium ion releases in the night magnetosphere at 9.5 and 7 Re, respectively, and over North and South America. The main spacecraft was to carry 12 ejectable ion release containers. Diagnostic measurements were to be made on the main spacecraft and on four ejectable sub-payloads. These sub-payloads total approximately 200 kg (~50 kg each). Optical measurements were to be made from the ground and from aircraft.

The scientific objectives were:

  • study of the plasma processes controlling the formation and decay of a magnetic cavity;
  • study of the momentum exchange with the ambient dilute plasma and of the long-range magnetoshperic perturbations generated thereby;
  • modification of the interaction of trapped energetic particles with self-generated whistler mode and ion cyclotron waves; and
  • tracing of acceleration and redistribution of the injected ions in the inner magnetosphere.

The spacecraft would have been battery powered, with a lifetime of less than 48 hours.

Firewheel was lost in the launch failure of the second Ariane-1. The technology developed for Firewheel was utilized some years later in the interantional AMPTE mission, especially with the German component IRM (AMPTE 3).

Nation: Germany
Type / Application: Research
Operator:
Contractors:
Equipment: ?
Configuration:
Propulsion: None
Power: Batteries
Lifetime: 2 days
Mass: 1080 kg (total); 880 kg (without subsatellites)
Orbit:
Satellite COSPAR Date LS Launch Vehicle Remarks
Firewheel (FIRE A) 1980-F01 23.05.1980 Ko ELA-1 F Ariane-1 with Firewheel Subsat 1, 2, 3, 4, AMSAT P3A, CAT 2