During 1994 the French national space agency, CNES, and the firm Matra Marconi, closely studied the requirements and benefits of an early warning satellite system. The latter's efforts culminated in a preliminary design featuring two 2,500-kg geosynchronous spacecraft which could be launched by the year 2005. The 600-kg payload would employ a cooled, solid-state array of cells sensitive to IR regime emissions within surface regions of 5 km2 extent. Position accuracies of up to 100 m at altitudes above 6 km should be achievable. The proposed spacecraft would be 3-axis-stabilized with a maximum electrical power capacity of 2kW, of which 0.4 kW would be required by the payload. Serious consideration of the proposals was expected in 1995 (References 83-84).
83. "ESAT", Flight International, 18-24 January 1995, p. 44.
84. "CNES Urged To Finance Missile Warning Study", Space News, 16-22 January 1995, p. 2.