UAV Directory - Aircraft Specification

Raytheon - Cobra

A developmental monoplane configuration aircraft with single tractor propeller. Work on the type commenced in 2005 with the objective of providing a more capable platform for sensor testing. The type secured initial US Federal Aviation Administration experimental certification in November 2006, the third awarded to a US developed UAV type, with five such certificates held by the type as at March 2007. Development continuing with the most recent declared test campaign occurring in North Dakota in June 2007.

View specification units in: METRIC | IMPERIAL

SPECIFICATION

Range Class: Tactical  
Airframe Monoplane with single tractor propeller  
Span 10.14 ft  
Length 9.25 ft  
Max take-off weight 99.21 lb  
Payload Weight 25.13 lb  
Cruise speed 60.00 kts  
Endurance 3hrs