Department of Energy
Required specifications for the Constant Hawk Aerial Surveillance Demonstration project contract award:
Specifications for contractor-provided aircraft to be used in demonstration:
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Fixed Wing, Single Engine Umanned Aerial Vehicle (UAV) with optional on-board pilot control.
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Federal Aviation Administration classification: Experimental.
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Minimum available payload weight (after installation of all UAV flight equipment): 600 pounds.
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Maximum gross (take-off) weight: less than 4,000 pounds.
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Minimum aircraft ceiling: 20,000 feet.
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Size and runway limits: less than 35 ft wingspan and less than 1,500 ft loaded takeoff distance.
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Payload access: removable aircraft under-frame for rapid removal and replacement of payload via ground jacks.
Personnel and UAV operation:
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Contractor must provide UAV ground control station compatible with specified aircraft and demonstrate past successful UAV operation using the specified aircraft and ground control station.
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Contractor must demonstrate past successful fully autonomous UAV landing (not remotely piloted).
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Contractor must provide evidence of prior successful flight systems engineering and integration projects, as well as demonstrate sufficient qualified personnel and facilities for aircraft/payload modifications and installations.
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Aircraft, contractor personnel, and all required facilities should be made available for completion of demonstration flight by Dec. 31, 2006.