A Tentative Fleet Plan
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Source: Norman Friedman's Seapower and Space p365-366.
AST.9003 envisaged satellites orbiting at 200 miles in 97 degree (sun-synchronous) orbits carrying two cameras with television readout, and an ELINT Antenna.
Resolution of the cameras would be 25 and 5 yards with swath widths of 45 and 7 miles respectively. It was expected that this system would provide 80% coverage of any given area within 2-3 months. The 25 yard camera would operate continuously, transmitting on command to 2-6 ground stations, with the narrow-field camera functioning on command.
ELINT would be used to intercept airborne communications, VHF radio relays (is Microwave links) and would search for ABM radars and UHF transmissions. The data would be transmitted via the imagery link, and could be correlated with images if the ELINT package used a directional antenna. If the TV link was eliminated in favour of film recovery, 20% of satellite weight could be saved, but the satellite would only last 10 days before it ran out of film.
Another system requirement was for accurate measurements of the satellite's orbits, either by radar, or by Doppler.
Friedman cites a Royal Navy analysis (ADM 1/28880, September 1963) that ships could barely be identified with the 25-yard resolution, with the 5-yard strip being too narrow for surveillance. To obtain sufficient coverage, 30 satellites in precise polar orbits would be required, with more being needed if precise orbits could not be maintained.
AST.9003 envisaged satellites orbiting at 200 miles in 97 degree (sun-synchronous) orbits carrying two cameras with television readout, and an ELINT Antenna.
Resolution of the cameras would be 25 and 5 yards with swath widths of 45 and 7 miles respectively. It was expected that this system would provide 80% coverage of any given area within 2-3 months. The 25 yard camera would operate continuously, transmitting on command to 2-6 ground stations, with the narrow-field camera functioning on command.
ELINT would be used to intercept airborne communications, VHF radio relays (is Microwave links) and would search for ABM radars and UHF transmissions. The data would be transmitted via the imagery link, and could be correlated with images if the ELINT package used a directional antenna. If the TV link was eliminated in favour of film recovery, 20% of satellite weight could be saved, but the satellite would only last 10 days before it ran out of film.
Another system requirement was for accurate measurements of the satellite's orbits, either by radar, or by Doppler.
Friedman cites a Royal Navy analysis (ADM 1/28880, September 1963) that ships could barely be identified with the 25-yard resolution, with the 5-yard strip being too narrow for surveillance. To obtain sufficient coverage, 30 satellites in precise polar orbits would be required, with more being needed if precise orbits could not be maintained.
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