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Primary function | high-altitude, long-endurance ISR
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Contractor | Northrop Grumman (Prime), Raytheon, L3 Comm
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Power Plant | Rolls Royce-North American F137-RR-100 turbofan engine
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Thrust | 7,600 pounds
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Wingspan | 130.9 feet (39.8 meters)
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Length | 47.6 feet (14.5 meters)
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Height | 15.3 feet (4.7 meters)
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Weight | 14,950 pounds (6,781 kilograms)
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Maximum takeoff weight | 32,250 pounds (14628 kilograms)
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Fuel Capacity | 17,300 pounds (7847 kilograms)
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Payload | 3,000 pounds (1,360 kilograms)
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Speed | 310 knots (357 mph)
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Range | 12,300 nautical miles
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Endurance | more than 34 hours
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Ceiling | 60,000 feet (18,288 meters)
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Armament | None
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Crew (remote) | three (LRE pilot, MCE pilot, and sensor operator)
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Sensors [Maritime Demonstration]
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Synthetic Aperture Radar (SAR) | 1.0/0.3 M Resolution (WAS/Spot)
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GMTI Radar | MDV 4.0 knots
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Maritime Search (MS) Radar | 15,000 sq. km/Min
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Maritime Target Acquisition (MTA) Radar | Cue for ISAR
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ISAR Radar | 3 Resolutions
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Electro-Optical | NIIRS 6.0/6.5 (WAS/Spot)
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Infrared | NIIRS 5.0/5.5 (WAS/Spot)
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Multi-Function Electronic Support (ES) | LR-100 (RWR, ESM, ELINT)
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Communications [Maritime Demonstration]
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Ku SATCOM Datalink | 1.5, 8.67, 20, 30, 40, 47.9 Mbps
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Dual Band CDL LOS (X, Ku) | 274 Mbps
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UHF SATCOM/LOS | Command and Control
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INMARSAT | Command and Control
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Initial operating capability | 2011 (Block 30); 2015 (Block 40)
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Inventory | active force, 33 (three more Block 30s purchased, to be fielded in 2017) (Current as of October 2014)
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