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the Army intended to meet division and corps level requirements. A gimbaled EO/IR sensor is used to
relay video in real time via a second airborne Hunter over a C-band LOS data link. Hunter deployed to
Macedonia to support NATO Balkan operations in 1999 and to Iraq in 2002. Although full-rate
production (FRP) was canceled in 1996, seven low-rate initial production (LRIP) systems of eight aircraft
each were acquired; an additional 18 aircraft were purchased in FY04 for delivery in FY05. All 18
aircraft will deliver as MQ-5s which have been modified to carry the Viper Strike and BLU 108
munitions. A competitively selected Extended Range/Multi-Purpose (ER/MP) UAS will begin to replace
Hunter as early as FY07. Hunter is expected to remain in service through 2009.
Characteristics:
RQ-5A MQ-5B RQ-5A MQ-5B
Length 22.6 ft 23 ft Wing Span 29.2 ft 34.25 ft
Gross
Weight
1,620 lb 1,800 lb Payload
Capacity
200 lb 200 lb
Fuel
Capacity
Moto Guzzi
421 lb
HFE 280 lb
Moto Guzzi
421 lb
HFE 280 lb
Fuel Type MOGAS JP-8
Engine Make Moto Guzzi (x2) Moto Guzzi
(x2)
Mercedez
HFE (x2)
Power 57 hp (x2) 57 hp (x2)
56 hp (x2)
Data Link LOS LOS Frequency C-band C-band
Performance:
Endurance 11.6 hr 18 hr Max/Loiter
Speeds
106/89 kt 106/89 kt
Ceiling 15,000 ft 18,000 ft Radius 144 nm 144 nm
Takeoff
Means
Runway Runway Landing Means Runway/Wire Runway/Wire
Sensor EO/IR EO/IR Sensor Make Tamam MOSP Tamam MOSP
SECTION 2 - CURRENT UA PROGRAMS
Page 7
UAS ROADMAP 2005
2.1.5 RQ-7A/B Shadow 200
User Service: Army
Manufacturer: AAI
Inventory: 100 + Delivered/332 Planned
Background: The Army selected the RQ-7 Shadow 200 (formerly tactical UA (TUA)) in December
1999 to meet the Brigade-level UA requirement for support to ground maneuver commanders.
Catapulted from a rail, it is recovered with the aid of arresting gear. Its gimbaled EO/IR sensor relays
video in real time via a C-band LOS data link. The first upgraded ‘B’ model was delivered in August
2004. The RQ-7B can now accommodate the high bandwidth tactical common data link (TCDL) and
features a 16 inch longer wingspan, 7 hours endurance (greater fuel capacity), and an improved flight
computer. Approval for FRP and IOC occurred in September 2002. Current funding allows the Army to
procure 63 systems of four aircraft each for the active duty forces and reserve forces. The Army’s
acquisition objective, with the inclusion of the Army Reserve component, is 88 total systems. Shadow
systems have been deployed to Iraq in support of GWOT and to South Korea.
Characteristics:
RQ-7A RQ-7B RQ-7A RQ-7B
Length 11.2 ft 11.2 ft Wing Span 12.8 ft 14 ft
Gross Weight 327 lb 375 lb Payload
Capacity
60 lb 60 lb
Fuel Capacity 51 lb 73 lb Fuel Type MOGAS MOGAS
Engine Make UEL AR-741 UEL AR-741 Power 38 hp 38 hp
Data Link(s) LOS C2 LOS C2 Frequency S-band
UHF
S-band
UHF
LOS Video LOS Video C-band C-band
Performance:
Endurance 5 hr 7 hr Max/Loiter
Speeds
110/70 kt 105/60 kt
Ceiling 14,000 ft 15,000 ft Radius 68 nm 68 nm
Takeoff Means Catapult Catapult Landing Means Arresting Wire Arresting Wire
Sensor EO/IR EO/IR Sensor Make Tamam POP 200 Tamam POP 300
SECTION 2 - CURRENT UA PROGRAMS
Page 8
UAS ROADMAP 2005
2.1.6 RQ-8A/B Fire Scout
User Service: Army and Navy
Manufacturer: Northrop Grumman
Inventory: 5 Delivered/192 Planned
Background: The Fire Scout Vertical Take-Off and Landing (VTOL) Tactical UAV (VTUAV) program
is currently in EMD. Five RQ-8A air vehicles and four ground control stations are now in developmental
testing. Over 100 successful test flights have been accomplished demonstrating autonomous flight,
TCDL operations, Multi-Mission Payload performance, and ground control station operations. The Army
selected the four-bladed RQ-8B model as its category IV UA for its future combat system (FCS) in 2003.
Planned delivery for the first two prototypes is in 2006. The Navy has selected the RQ-8B to support the
Littoral Combat Ship (LCS) class of surface vessels. http://uav.navair.navy.mil/.
Characteristics:
RQ-8B RQ-8B
Length 22.9 ft Wing Span 27.5 ft
Gross Weight 3,150 lb Payload Capacity 600 lb
Fuel Capacity 1,288 lb Fuel Type JP-5/JP-8
Engine Make Rolls Royce 250-C20W Power 420 shp
Data Link(s) LOS C2 Frequency Ku-band/UHF
LOS Video Ku-band
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
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unmanned aircraft systems roadmap(12)
