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X-47 Pegasus

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Background: Northrop Grumman built the X-47/Pegasus unmanned combat aerial vehicle (UCAV) demonstrator under a $12 million DARPA/Navy contract. It is intended to evaluate technologies and concepts for a possible follow-on carrier-capable, naval UCAV (UCAV-N) for fielding in the post-2010 timeframe. The UCAV-N is to perform three missions: surveillance, strike, and suppression of enemy air defenses (SEAD). The single X-47 flight test aircraft was formally rolled out in July, 2001. The first of a twelve-flight test program is anticipated to begin in late 2001.

Characteristics:

Length, ft 27.9 Wing Span, ft 27.8
Gross Weight, lbs 5,500 Payload Weight, lbs 1,000
Fuel Capacity, lbs 1,580 (1,040 mission) Fuel Type JP
Engine Make P&W JT15D-5C-TF Power, lbs 3,190
Structure Composite/aluminum  
Guidance   Navigation GPS/INS
Data Link(s) LOS only Data Rate(s)  

Performance:

Endurance, hrs 1.0+ Radius, nm  
Max Speed, kts   Stall Speed, kts  
Altitude, ft    
Takeoff Means Conventional  
Navigation Preprogrammed /
direct control
 
Landing Means Conventional  

Sensor(s):