airdft defensetechs
Post on 05-Apr-2018
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AirMule: Unprecedented capabilities, extraordinary AirMule: State of the Art components and Urban’s patented,
LEADING THE FANCRAFT REVOLUTION
AIRDFT : REVOLUTIONARY CAPABILITIES FOR TODAY’S
BATTLEFIELDAND TOMORR OW’S CHALLENGES
AIRDFT: BEYOND THE BATTLEFIELD
Our Partner family of aircraft r epresent a true r evolution in
VTOL technology. Our partner paten ted, aerodynamic
innovations radically transform basic d ucted -fan
configurations into uniquely stable and maneuverable air craft
that can r each speeds of betwee n 100 to 140 kts and carry
significant paylo ads for up to 5 hours. With their shr ouded
rotors and small footprint, Fancraft are uniquely suitedto
urban and obstructed environments.The present ‘family’
includes the single engined “AirDFT” Cargo and
DFTEvac UAS, its manned va riant, and the lar ger ,
twin-engined “X-Hawk”, a 10 passen ger version. All have both
civil and military applications. AirDFT, our partner flagship
aircraft, is currently undergoing flight testing.
Today’s battlefield is increasingly defined by an enemy whose
unconventional tactics seriously challenge conventional
technologies. Tomorr ow’s battlefield will undoubtedly be mor e
so. Cities and obstructed or inaccessible environmentsare the
insurgent’s battlefield of choice. Supply convoys and medical
teams entering these locations are under constant thr eats
unlike any that have been experienced in the past. IEDs and
r oof-launched RPGs are an ever more lethal force against
humvees, trucks and helicopters. AirDFT, a tactical
Unmanned Aerial System (UAS) can help combatants r eclaim
an essential edge by enabling precise point to point support
and DFTEvac solutions in battle cond itions that are incr eas-
ingly averse to conventional r otor craft access.
AirDFT’s small visual footprint, low noise and r educed IR
signature offer a stealth advantage that greatly enhances its
effectiveness and survivability. Unmatched time to target with
the unprecedented capability of DFTEvac on r eturn offers life
saving potential. Simplicity of design without a complex cyclic
r otor head means high reliability and low operating cost.
AirDFT offers much needed capabilities to emergency
r esponders in the most challenging situations such as
earthquakes and floods. The ability to quickly deliver water ,
food and medica l supplies directly to affected popula tions--
no matter how isolated--can save lives. During nuclear ,
biologic al or chemical emergencies AirDFT offers transfor ma-
tive assessment and r esponse capabilities. Day to day
multiple mission capability (electric grids, bridge inspect ion,
agricultural spraying, of fshor e oil platfor m support to n ame a
few) makes AirDFT a co st effective addition to any commer-
cial helicopter fleet.
AIRDFT UNMANNED AERIAL SYSTEM
SPECIFICATIONS (2 EQUIPPED AIRDFT 2 UAS):
Weights Empty Weight Max Load (Fuel+Payload)
1,700 lbs
1,400 lbs (771 kg)(635 kg)
Fuel Consumption (65 kts) (100 kts)
290 lbs/hr (132 kg/hr)
360 lbs/hr (163 kg/hr) Max Gross Takeoff Weight 3,100 Ibs (1,400 kg)
Performance Engine Power (Turbomeca Arriel 2)Max Speed (Dash) Max Altitude FlightEndurance (Depending
on useful load)
Dimensions Fuselage size (feet)
(meters) Rotor Diameter
940 SHP 100 kts (180 km/hr) 12,000 feet Up to 5 hrs
22.3L x 7.1W x 5.9H 6.2L x 2.15W x 1.8H
5.9 ft (1.8 m)
Note: Above estimates are preliminary and subject to change
es
R evolution
Vertical mobility in urban envir onments
Extremely cost ef fective
All weather capability
Numerous tactica l r oles
CH-53, EH-101 and truck transportable
Unmatched time to target, “on-demand”, obstacle fr ee
delivery of supplies
Evacuation of casualties with no risk to ground personnel
Reduced r eliance on vulnerable supply convoys
Ideal for IED neutralization; minimal,autonomous
operational infrastructur e
Greater infantry agility through the r eduction of load
carrying r equir ements
Equivalent of f-shor e missions from Navy frigates and small
vessels, both Civil and Military
Numerous civil emergency and disaster r esponse
applications (Homeland Security, floods, earthquakes,
compromised nuclear facilities)
Composite structur e
Fly by Wir e
100% aerospace grade components
FCS fully mil-spec qualified, quad-redundant, running on
Integrity OS DO178 certifiable
Designed to meet existing FAA standards (primarily
FAR part 27)
Patented Vane Control System offering an unpr ecedented
six, de-coupled degrees of fr eedom capability
Patented adaptable (louvered) ducts enabling speeds in
excess of 100 kts
Patented aerodynamically tailored fuselage generates in
excess of 50% of lift in forward flight
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