Performance:
Endurance 6+ hr Max/Loiter Speeds 125/0 kt
Ceiling 20,000 ft Radius 150 nm
Takeoff Means Vertical Landing Means Hover
Sensor EO/IR/LDRF Sensor Make FSI Brite Star II
SECTION 2 - CURRENT UA PROGRAMS
Page 9
2.1.7 MQ-9 Predator B
User Service: Air Force Manufacturer: General Atomics Aeronautical Systems Inc. Inventory: 6 Delivered/60 Planned
Background: The MQ-9 is a medium-to-high altitude, long-endurance unmanned aircraft system. Its primary mission is as a persistent hunter-killer for critical time sensitive targets and secondarily to act as an intelligence collection asset. The MQ-9 system consists of four aircraft, a ground control station (GCS), and a Predator Primary Satellite Link. The integrated sensor suite includes a moving target-capable synthetic aperture radar (SAR) and a turret that houses electro-optical and mid wave infrared sensors, a laser range finder, and a laser target designator. The crew for the MQ-9 is one pilot and one sensor operator. The USAF proposed the MQ-9 system in response to the Department of Defense request for Global War On Terrorism (GWOT) initiatives, in October 2001. In June 2003, Air Combat Command (ACC) approved the MQ-9 Concept of Operations. The objective force structure includes nine combat-coded systems and 36 aircraft. ACC approved the final basing decision to put the MQ-9 squadron at Indian Springs Air Force Auxiliary Field in February 2004.
http://www.af.mil/factsheets/factsheet_print.asp?fsID=122&page=1.
Characteristics:
MQ-9 A MQ-9 A
Length 36 ft Wing Span 66 ft
Gross Weight 10,500 lb Payload Capacity *750 lb
Fuel Capacity 4,000 lb Fuel Type JP
Engine Make Honeywell TPE 331-10 Power 900 shp
Data Link(s) BLOS Frequency Ku-band
LOS C-band
* Up to 3,000 lb total externally on wing hardpoints.
Performance:
Endurance 30 hr/clean 16-20 hr/external stores Max/Loiter Speeds 225/TBD kt
Ceiling 50,000 ft Radius 2,000 nm
Takeoff Means Runway Landing Means Runway
Sensor EO/IR Sensor Make MTS-B
SAR/MTI Weapons Four, 500 lb class or 8-10, 250 lb class
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