AF.mil  
Join the Air Force

Information > Factsheets > MQ-1 Predator

MQ-1 PREDATOR
At day's end
View All Media
Next Image
Download

Fact Sheet Tools
 Printable Fact Sheet


Mission
The MQ-1 Predator is a medium-altitude, long-endurance, unmanned aircraft system  The MQ-1's primary mission is interdiction and conducting armed reconnaissance against critical, perishable targets. When the MQ-1 is not actively pursuing its primary mission, it acts as the Joint Forces Air Component Commander-owned theater asset for reconnaissance, surveillance and target acquisition in support of the Joint Forces commander.

Features
The MQ-1 Predator is a system, not just an aircraft. A fully operational system consists of four aircraft (with sensors), a ground control station, a Predator Primary Satellite Link, or PPSL, along with operations and maintenance crews for deployed 24-hour operations.

The basic crew for the Predator is a pilot, sensor operator and mission intelligence coordinator. They fly the aircraft from inside the ground control station via a line-of-sight data link or a satellite data link for beyond line-of-sight flight. The aircraft is equipped with a color nose camera (generally used by the pilot for flight control), a day variable-aperture high resolution TV camera, a variable-aperture infrared camera (for low light/night), and other sensors as the mission requires.  The cameras produce full-motion video.

The MQ-1 Predator carries the Multi-spectral Targeting System which integrates electro-optical, infrared, laser designator and laser illuminator into a single sensor package. The aircraft can employ two laser-guided AGM-114 Hellfire anti-tank missiles.

The system is composed of four major components which can be deployed for worldwide operations. The Predator aircraft can be disassembled and loaded into a container for travel. The ground control system is transportable in a C-130 Hercules (or larger) transport aircraft or installed in a fixed facility. The Predator can operate on a 5,000 by 75 feet (1,524 meters by 23 meters), hard surface runway with clear line-of-sight. The ground data terminal antenna provides line-of-sight communications for takeoff and landing. The PPSL provides over-the-horizon communications for the aircraft.

An alternate method of employment, Remote Split Operations, employs a smaller version of the ground control system called the Launch and Recovery GCS, or LRGCS. This system conducts takeoff and landing operations at the forward deployed location while the CONUS based ground control system conducts the mission via extended communication links.

The aircraft includes an ARC-210 radio, an APX-100 IFF/SIF with Mode 4, and an upgraded turbo-charged engine. The latest upgrade, which enhances maintenance and performance, includes dual nose cameras, split engine cowling, steel braided hoses and improved engine blocks.

Background
The "M" is the Department of Defense designation for multi-role and "Q" means unmanned aircraft system. The "1" refers to the aircraft being the first of a series of purpose-built remotely piloted aircraft systems.

The Predator system was designed in response to a Department of Defense requirement to provide persistent intelligence, surveillance and reconnaissance information to the warfighter.

In April 1996, the secretary of defense selected the U.S. Air Force as the operating service for the RQ-1 Predator system. A change in designation from "RQ-1" to "MQ-1" occurred in 2002 with the addition of the armed reconnaissance role.

Operational squadrons are the 15th and 17th Reconnaissance Squadrons at  Creech Air Force Base, Nev.  The 11th RS provides formal upgrade training also at Creech AFB.

General Characteristics
Primary Function: Armed reconnaissance, airborne surveillance and target acquisition
Contractor: General Atomics Aeronautical Systems Incorporated
Power Plant: Rotax 914F four cylinder engine
Thrust: 115 horsepower
Wingspan: 55.25 feet (16.8 meters)
Length: 27 feet (8.22 meters)
Height: 6.9 feet (2.1 meters)
Weight: 1,130 pounds ( 512 kilograms) empty
Maximum takeoff weight:  2,250 pounds (1,020 kilograms)
Fuel Capacity: 665 pounds (100 gallons)
Payload: 450 pounds (204 kilograms)
Speed: Cruise speed around 84 mph (70 knots), up to 135 mph
Range: up to 400 nautical miles (454 miles)
Ceiling: up to 25,000 feet (7,620 meters)
Armament: two laser-guided AGM-114 Hellfire missiles 
Crew (remote):
  Three (pilot, sensor operator, and mission intelligence coordinator)
Initial operational capability: March 2005
Unit Cost: $20 million (fiscal 2009 dollars) (includes four aircraft, ground control stations, and Predator Primary Satellite Link)
Inventory: Active force, 130; ANG, 8; Reserve, 0


Point of Contact
Air Combat Command, Public Affairs Office; 130 Andrews St., Suite 202; Langley AFB, VA 23665-1987; DSN 574-5007 or 757-764-5007; e-mail: accpa.operations@langley.af.mil


November 2009




 Inside AF.mil

ima cornerSearch

ima cornerUASs/RPAs

 BQM-167A Air Force Subscale Aerial Target
MQ-1 Predator
MQ-9 Reaper
QF-4 Drone
RQ-11B Raven
RQ-170 Sentinel
RQ-4 Global Hawk
Scan Eagle
Wasp III




Site Map      Contact Us     Questions     Security and Privacy notice     E-publishing