Engineering:AeroVironment RQ-14 Dragon Eye

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RQ-14 Dragon Eye
US Navy 050627-N-0295M-096 A Dragon Eye Unmanned Aerial Vehicle (UAV) on display at the 2005 Naval UAV Air Demo held at the Webster Field Annex of Naval Air Station Patuxent River.jpg
Role Remote controlled UAV[1]
Manufacturer AeroVironment
First flight June 2001
Introduction Mid-2002
Primary user United States Marine Corps

The AeroVironment RQ-14 Dragon Eye is a small reconnaissance miniature UAV developed by the Naval Research Laboratory and the Marine Corps Warfighting Laboratory for use by the United States Marine Corps.

Design and development

A marine checks a DE-903 UAV

It is a tailless design with a rectangular wing and twin props. It is designed to fit into a backpack, with a weight of 5 pounds (2.3 kilograms) and a span of 3 feet 9 inches (1.14 meters). It can be launched by hand or using a store-bought bungee cord. It also uses a break-apart system to increase durability—parts of the plane break apart instead of shattering and can be reattached later or replaced with new parts. It has a GPS-INS-based waypoint navigation system.

The operator monitors Dragon Eye operation through "video goggles" connected to a laptop computer. The control system weighs about 12 pounds (5.4 kilograms).

The Dragon Eye aircraft is used primarily for scouting urban areas, and is especially useful in urban assaults. Its camera, when used with a trained Marine, can be used to spot enemies without alerting them to the UAV's presence.

The production contract for Dragon Eye was awarded to AeroVironment in 2003, and over 1000 aircraft were built before the Marines switched over to another UCAV of AeroVironment (RQ-11 Raven B) for the remainder of the Dragon Eye production contract.

The Dragon Eye has been used in Iraq, post-invasion, from 2003–present.

General characteristics

A Dragon Eye UAV

Data from Dragon Eye data sheet[2]

General characteristics

  • Length: 3 ft (0.91 m)
  • Wingspan: 3.75 ft (1.14 m)
  • Gross weight: 5.9 lb (2.7 kg)

Performance

  • Cruise speed: 40 mph (64 km/h, 35 kn)
  • Range: 3.1 mi (5.0 km, 2.7 nmi)
  • Endurance: 45-60 minutes
  • Service ceiling: 300–500 ft (91–152 m)
  • Transmission range: 6.2 mi (10.0 km)

References

External links