[email protected] www.defensetechs.com AirMule: Unprecedented capabilities, extraordinary AirMule: State of the Art components and Urban’s patented, LEADING THE FANCRAFT REVOLUTION AIRDFT : REVOLUTIONARY CAPABILITIES FOR TODAY’S BATTLEFIELDANDTOMORR OW’S CHALLENGES AIRDFT: BEYOND THE BATTLEFIELD Our Partner family of aircraft r epresent a true r evolutionin 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”, a10 passen ger version. All have both civil and military applications. AirDFT, our partner flagship aircraft, is currentlyundergoing flight testing. Today’s battlefield is increasingl y defined by an enemy whose unconventionaltactics seriously challenge conventional technologies. Tomorr ow’s battlefield will undoubtedly be mor e so. Cities and obstructed or inaccessible environments are 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 AirDFTa 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 Flight Endurance (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 mobilityin 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 faciliti es) Composite structur e Fly by Wir e 100% aerospace grade components FCS fully mil-spec qualified, quad-redundant, running on IntegrityOS DO178 certifiable Designed to meet existing FAAstandards (primarily FAR part 27) Patented Vane Control System of fering 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 f uselage generates in excess of 50% of lift in forward flight