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high wing, Radio Controlled or computer assisted autopilot UA capable of daylight or infrared
reconnaissance and other related missions. Although it is a relatively new aircraft, the recent
modifications that included the addition of navigation/strobe lights, a Mode C transponder, dual GCS
operational capability, and a new high resolution digital camera, made it a success during support to OIF.
Characteristics:
XPV-2 XPV-2
Length 9.11 ft Wing Span 12.8 ft
Gross Weight 130 lb Payload Capacity 30 lb
Fuel Capacity 5 gal Fuel Type MOGAS/oil
Engine Make 3W 100cc Power 9.5 hp
Data Link(s) C2 Frequency VHF/UHF
Video L-band Video Downlink
Performance:
Endurance 8.5 hr Max/Loiter Speeds 75/50 kt
Ceiling 10,000’MSL Radius 40 NM
Takeoff Means Runway Landing Means Runway
Sensor EO/IR Sensor Make BAI
SECTION 2 - CURRENT UA PROGRAMS
Page 23
UAS ROADMAP 2005
2.3.5 CQ-10 SnowGoose
User Service: USSOCOM, Army
Manufacturer: MMIST Inc.
Inventory: 15 Delivered/TBD Planned
Background: USSOCOM selected the CQ-10A SnowGoose to dispense leaflets for Psychological
Operations (PSYOP), deliver small supply bundles to Special Operations Forces, provide aerial
surveillance and communications relay capabilities. The SnowGoose is a powered, programmable, GPSguided
parafoil with modular payload bays that can carry up to six individual payload or fuel bins. The
SnowGoose can be ground launched from a HMMWV or air-deployed from a C-130, C-141, or C-17 at
altitudes up to 25,000 feet. From the ground, it can climb to 18,000 feet. It can carry up to 575 pounds of
leaflets, supplies, or other fixed cargo payloads with an endurance of 1-3 hours or it can stay aloft with a
75 pound payload for 14-16 hours. (Note: Endurance is a function of the selection of ground launch or
air launch parachute kit, with greater endurance achieved in its ground launch configuration). The
SnowGoose is designed to operate with only four operators with a turn-around time of less than four
hours between uses. The SnowGoose was originally developed as the Wind Supported Aerial Delivery
System (WSADS) and refined in the Air-Launched Extended Range Transporter (ALERT) ACTD. The
first flight occurred in April 2001, and IOC was achieved in Jan 2005.
Characteristics:
CQ-10A CQ-10A
Length 9.5 ft Wing Span 6.8 ft
Gross Weight 1,400 lb fully loaded Payload Capacity 575 lb
Fuel Capacity Up to 91 U.S. gal Fuel Type MOGAS/AVGAS
Engine Make Rotax 914 UL Power 110 hp
Data Link(s) LOS/BLOS C2 Frequency L-band
LOS Video
Performance:
Endurance Up to 19 hr
(Maximum), 9-11 hr
with 200 lb cargo
Max/Loiter Speeds 33/33 kt
Ceiling > 18,000 ft Radius 160 nm
Takeoff Means Airdrop/Truck Launch Landing Means Parafoil
Sensor Configurable Sensor Make n/a
SECTION 2 - CURRENT UA PROGRAMS
Page 24
UAS ROADMAP 2005
2.3.6 Onyx Autonomously Guided Parafoil System
User Service: Army (USSOCOM)
Manufacturer: Atair Aerospace, Inc.
Inventory: 5 Delivered/5 Planned
Background: Onyx is an autonomously guided parafoil system developed by
the U.S. Army Natick Soldier Center (NSC). Onyx systems are air-deployed
from a C-130, C-141, or C-17 at up to 35,000 ft., autonomously glide over 30
miles, and land cargo within 150 ft. of a target. Cargo for ground and special
operations forces includes food and water, medical supplies, fuel, munitions and
other critical battlefield payloads. Onyx includes advanced capabilities such as
flocking (formation flying), active collision avoidance, and adaptive control (selflearning
functions). With this technology, multiple systems (50+) can be
deployed in the same airspace, guiding payloads to one, or multiple targets without possibility of midair
collisions. Smaller versions have been developed to precisely deliver sensors or submunitions.
Characteristics:
Onyx Onyx
Length 45 ft Wing Span 38 ft
Gross Weight 2,300 lb Payload Capacity 2,200 lb
Fuel Capacity N/A Fuel Type N/A
Engine Make N/A Power N/A
Performance:
Endurance Varies Max/Loiter Speeds 0/70 kt
Ceiling 35,000 ft Radius 30 nm
Takeoff Means Airdrop Landing Means Parafoil
SECTION 2 - CURRENT UA PROGRAMS
Page 25
UAS ROADMAP 2005
2.4 SMALL UAS
2.4.1 Mini UA
Dragon Eye FPASS Pointer Raven BUSTER
Manufacturer AeroVironment Lockheed Martin AeroVironment AeroVironment Mission
Technologies,
Inc.
User Service Marine Corps Air Force SOCOM, AF Army, SOCOM,
AF
Night Vision
Labs, US Army
Weight 4.5 lb 7 lb 8.3 lb 4 lb 10 lb
Length 2.4 ft 2.7 ft 6 ft 3.4 ft 41 inches
Wingspan 3.8 ft 4.3 ft 9 ft 4.3 ft 49.5 inches
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unmanned aircraft systems roadmap(18)
