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Characteristics:
Eagle Eye Eagle Eye
Length 17 ft Rotor Span 15.2 ft
Gross Weight 2,850 lb Payload Capacity 200-300 lb
Fuel Capacity 832 lb Fuel Type JP/Diesel
Engine Make P&W 200-55 Power 641 hp
Data Link(s) LOS C2/Video LOS C2 Frequency Ku-Band/S-Band
Performance:
Endurance 5.5 hr Max/Loiter Speeds 210/97 kt
Ceiling 20,000 ft Radius 110 nm w/3 hr TOS
Takeoff Means Hover Landing Means Hover
Sensor MMR Sensor Make Telephonics 1700-CG
EO/IR FSI Star Safire III
SECTION 2 - CURRENT UA PROGRAMS
Page 19
UAS ROADMAP 2005
2.3 SPECIAL OPERATIONS UAS
2.3.1 Neptune
User Service: Navy
Manufacturer: DRS Unmanned Technologies
Inventory: 15 Delivered/27 Planned
Background: Neptune is a new tactical UA design optimized for at-sea launch and recovery. Carried in
a 72x30x20 inch case that transforms into a pneumatic launcher, it can be launched from small vessels
and recovered in open water. It can carry IR or color video sensors, or can be used to drop small
payloads. Its digital data link is designed to minimize multipath effects over water. First flight occurred
in January 2002, and an initial production contract was awarded to DRS Unmanned Technologies in
March 2002.
Characteristics:
Neptune Neptune
Length 6 ft Wing Span 7 ft
Gross Weight 80 lb Payload Capacity 20 lb
Fuel Capacity 18 lb Fuel Type MOGAS
Engine Make 2 Stroke Power 15 hp
Data Link(s) LOS C2 Frequency UHF
LOS Video UHF
Performance:
Endurance 4 hr Max/Loiter Speeds 84/60 kt
Ceiling 8,000 ft Radius 40 nm
Takeoff Means Pneumatic Landing Means Water/Skid/Parachute
Sensor EO or IR Sensor Make DRS
SECTION 2 - CURRENT UA PROGRAMS
Page 20
UAS ROADMAP 2005
2.3.2 Maverick
User Service: DARPA/Army/Navy
Manufacturer: Boeing/Frontier/Robinson
Inventory: 4 Delivered/5 Planned
Background: Maverick is an unmanned version of the Robinson R22 helicopter. Frontier modified it in
1999 to serve as a testbed for developing the control logic for their DARPA A-160 UA effort.
Subsequently, the Navy decided to acquire four Mavericks in 2003.
Characteristics:
Maverick Maverick
Length 28.8 ft Rotorspan 25.2 ft
Gross Weight 1,370 lb Payload Capacity 400 lb
Fuel Capacity 100 lb Fuel Type AVGAS
Engine Make Lycoming 0-360-J2A Power 145 hp
Data Link(s) TBD Frequency TBD
Performance:
Endurance 7 hr Max/Loiter Speeds 118/0 kt
Ceiling 10,800 ft Radius 175 nm
Takeoff Means Hover Landing Means Hover
Sensor EO/IR Sensor Make Wescam
SECTION 2 - CURRENT UA PROGRAMS
Page 21
UAS ROADMAP 2005
2.3.3 XPV-1 Tern
User Service: SOCOM
Manufacturer: BAI Aerosystems
Inventory: 65 Delivered/65 Planned
Background: Originally an Army testbed for a fiber-optic guided UA, Tern was completely retooled in
late 2001 to give it a larger, steerable nose gear and main gear fitted with tires suitable for rough terrain
with electronically-actuated disc brakes to aid short-field recovery that enabled the aircraft to carry a
belly-mounted dispensing mechanism. Tern was operated in support of Special Operations Forces by
Navy personnel from Fleet Composite Squadron Six (VC-6, previously the USN's Pioneer UA Squadron)
in Afghanistan to perform force protection missions and to dispense an unattended ground sensor
weighing over 20 pound. Over 225 combat hours were flown during two 3-month long deployments. In
early 2004, a Tern variant was developed that eliminated the landing gear and incorporated skids and a
tail-hook. A marinized control station was developed, and the system was successfully demonstrated
onboard a Navy LPD (USS Denver). The reduced drag of the skid/tailhook recovery system improved
the vehicle's mission endurance from 4 to over 6 hours.
Characteristics:
XPV-1 XPV-1
Length 9.0 ft Wing Span 11.4 ft
Gross Weight 130 lb Payload Capacity 25 lb
Fuel Capacity 28 lb Fuel Type MOGAS/oil
Engine Make 3W 100 cc Power 12 hp
Data Link(s) LOS C2 Frequency L/S-band
LOS Video UHF
Performance:
Endurance 2 hr Max/Loiter Speeds 87/50 kt
Ceiling 10,000 ft Radius 40 nm
Takeoff Means Runway Landing Means Runway
Sensor EO or IR Sensor Make BAI PTZ
SECTION 2 - CURRENT UA PROGRAMS
Page 22
UAS ROADMAP 2005
2.3.4 XPV-2 Mako
User Service: SOCOM
Manufacturer: NAVMAR Applied Sciences Corporation/BAI Aerosystems
Inventory: 30 Delivered/30 Planned
Background: Mako is a lightweight long endurance versatile unmanned aircraft capable of a variety of
missions, yet of sufficiently low cost to be discarded after actual battle, if necessary. It is a single engine,
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unmanned aircraft systems roadmap(17)
