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Tournesol / Polaire (D 2A)

Tournesol [CNES]

The scientific mission of Tournesol was to detect the probable presence of hydrogen in several directions of the celestial sphere. Scientific and technological data recorded by an onboard recorder were transmitted on command. The satellite was a cylinder 70 cm in diameter and 80 cm long. The rotating axis was directed parallel to the sun-satellite axis, with an accuracy of about 10-20 min of arc. The spin rate was 1 rpm.

  • Atomic Hydrogen and Oxygen Spectrophotometer
  • Lyman-Alpha Analyzer

The Polaire spacecraft mission was to be complementary to that of Tournesol, except the orbit was to be more polar (I=75 vs 45 deg) and H-Ly-Beta emissions observed (instead of H-Ly-Alpha) in the vicinity of 600 km.

Nation: France
Type / Application: Science
Operator: CNES
Contractors:
Equipment:
Configuration:
Propulsion:
Power: 4 deployable fixed solar arrays, batteries
Lifetime:
Mass: 96 kg
Orbit: 456 km × 702 km, 46.4° (Tournesol);
Satellite COSPAR Date LS Launch Vehicle Remarks
Tournesol (D 2A) 1971-030A 15.04.1971 Ko ELD Diamant-B
Polaire (D 2A) 1971-F14 05.12.1971 Ko ELD F Diamant-B