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The standard ScanEagle is operating on Intelligence, Reconnaissance
and Surveillance missions, supporting US and Australian forces.
It is operated by Boeing under outsourcing contracts awarded by
the US Marine Corps and Australian government. In those missions
these UAVs have accumulated over 50,000 hours of operational experience
operating primarily in Iraq and Afghanistan.
Using
the basic ScanEagle aerial vehicle design, Boeing designed a biological
combat assessment system (BCAS), to meet requirements defined by
the Defense Threat Reduction. Such system will be able to collecting
data on biological hazards, to identify and assess hostile threats.
The system will employ new technologies to monitor sites suspected
of containing weapons of mass destructions targets. When such targets
are attacked by friendly forces, the BCAS will attempt to locate,
track and collect biological warfare agents released into the air
during air strikes. The BCAS system will integrate both ISR and
Biological Collection and Detection (BC) versions of ScanEagle.
The ISR vehicle will use electro-optical and infrared cameras to
observe a strike and resultant plume. This data will be used to
create a predictive dispersal model, guiding the BC aircraft to
collect samples from the plume of airborne agents. Each BC ScanEagle
will mount five modular cartridges and four 'pass through' particle
collectors, enabling multiple measurements. It will also have a
plume sensor to monitor the relevant target. Controlled via satellite
link the two UAVs will be able to reach targets over a distance
of 250 nautical miles, loiter over the area for 60 minutes.
Another derivative of the ScanEagle,
currently pursued by Boeing is the 'ScanEagle Compressed Carriage'
(SECC) design. Using air durfaces and fuselage derived from the
dominator program and avionics, payloads and controls of the ScanEagle,
this vehicle is planned for air insertion or launch from submarines.
In air insertion, the vehicle is extracted from the aircraft by
a parachute. As the parachute decelerates it to the required altitude
and speed, SECC will separate from the parachute, deploy its wings
and start the engine to begin the mission. When launched from a
submarine, SECC will use a sealed sub-scale container to launch
from a Trident missile-launch tube. Once airborne, the container
will open, starting the vehicle's deployment sequence.
SECC utilize many elements derived from 'Dominator', another
Boeing program developed by Boeing for the US Air Force Research
Lab's (AFRL) area dominance munition technology program. SECC
uses folding flight surfaces, along with container-loaded
design optimized for internal carriage by cargo aircraft or
for external carriage by fighters, using standard weapon's
carriage mounts. These vehicles could also use the 'wingtip
snag' for airborne recovery by transport aircraft, tilt-rotors
or helicopters.
Multiple SECCs will be able to operate in constellations,
controlled by a single ground station on long-range ISR missions,
extended pursuit of high-priority, time sensitive targets,
active and passive information warfare operations and monitoring
and surveillance of areas affected by weapons of mass destruction.
ScanEagle was developed in partnership with Boeing. The system
was designed for field operations by land or sea, utilizing the
SuperWedge launcher and patented SkyHook retrieval system. The air
vehicle has a tubular fuselage, coupled with a large wing (10.2'
wing span) with winglets used as vertical rudders. ScanEagle has
an empty weight of 26.5 pounds (12 kg) and maximum takeoff weight
of 44 lbs (20 kg). It is designed for cruising speed of 48 kt and
operates at a ceiling of 19,500 ft. for missions extending over
20 hours. The UAV uses an inertial stabilized electro-optical turret
using visual or infrared cameras. The ScanEagle uses a 1.9 hp two
stroke engine running on gasoline. A heavy fuel engine running on
JP-5 is in development. This engine will extend mission endurance
over 28 hours.
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