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Penguin B Datasheet Performance:Datasheet V 2.0 Sleek and Efficient Design Gives Best in Class Performance

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Penguin B Datasheet Performance:Datasheet V 2.0 Sleek and Efficient Design Gives Best in Class Performance Penguin B Datasheet Performance:Datasheet v 2.0 Sleek and efficient design gives best in class performance. Optimized for endurance, UNMANNED PLATFORMS Penguin has enough internal volume to lift 7.5 liters of fuel which will provide 20+ hours UNMANNED PLATFORMS PENGUIN B UAV PLATFORM AND SUBSYSTEMS PENGUIN B UAV PLATFORM AND SUBSYSTEMS endurance with the fuel injected engine. The optimized high lift flap system provides stall speeds of <13 m/s, while giving excellent flight handling qualities due to a well designed V- tail geometry. MeetingDatasheet your v 2.0 mission requirements: STEP 1 Configure Penguin B UAV Factory recommends UNMANNED PLATFORMS PENG• SelectU yourIN engine B type U andA onboardV generatorPLA TFORM Penguin B® platform usingAPenguin NPiccoloD SUB BS autopilotplYSatformTEMS • Select takeoff method ready for payload and systemsready from for payloadCloud Cap and • Select landing gear type autopilot integration Technologyautopilot. Penguin integration B • Select fuel tank volume and fuel level sensors 2 autopilot20+ hourconfiguration endurance files2 20+ hour endurance • Select Pitot type are available at no cost to Penguin B• SelectOverview transportation packaging type Fuel injected engine all PenguinFuel injected B and engine Piccolo Penguin'sPenguin B is• philosophy: Adda high-performance additional accessories, semi-integrated spare parts andsmall options UAV platform available option Penguin's philosophy: users.option Designedfor final asassembly a high performanceand customization unmanned by aircraft,UAV system Penguin integrators. B is capable Penguin of up to 26.5 DesignedSTEP 2 as Gettinga high performance autonomous unmanned aircraft, Penguin B is capable of up to 26.5 UpPenguin to 10 Bkg pl payloadatform hourB is capableendurance of upwith to the 26.5 4 kghour payload. endurance With awith small the footprint 4 kg payload. of 3.3 meter With awingspan, Up to 10 kg payload hour endurance• Integrate with the the 4 autopilotkg payload. and Withdata-link a small system footprint of your of choice3.3 meter wingspan, capacityready for payload and Penguinsmall footprint B can ofhandle 3.3 meter up to wingspan,11.5 kg of Penguincombined B fuel can and handle payload up toweight. 11.5 kg Modular of capacity Penguin B can• Install handle payload up to of 1 1.5your kg choice of combined fuel and payload weight. Modular autopilot integration compositecombined structure, fuel and fastpayload assembly weight., large Modular access hatches,composite removable structure, payload fast bayassembly, are the, 80 W power from compositelargeSTEP access 3 structure,Start hatches, performing fast assemblyremovable your, large payloadmission access bay, hatches, are the removable key features payload of baythe, are the 80 W power from 2 key features of the Penguin B innovative design. onboard20+ hour generator endurance key features of the Penguin B innovative design. onboard generator Penguin B innovative design. Penguin B allows customers to kick-start small system Afixedvailable wing as anUAV airframe production ready forwith the the autopilot use ofand an payload industry-proven integration. airframe and Fuelsystem injected engine Dimensions:Penguin'sAvailable as an philosophy: airframe ready for the autopilot and payload integration. ® superior subsystems and components. Freeoption Piccolo® autopilot Free Piccolo autopilot Designed as a high performance unmanned aircraft, Penguin B is capable of up to 26.5 CADconfiguration model of Penguin files B Upconfiguration to 10 kg payload files hourSpecifications: endurance with the 4 kg payload. With a small footprint of 3.3 meter wingspan, available to simplify the Specifications: Catapult,capacity car-top or Penguin B can handle up to 11.5 kg of combined fuel and payload weight. Modular payloadCatapult, and autopilot car-top or Parameter Value runway takeoff compositeParameter structure, fast assembly, large accessValue hatches, removable payload bay, are the runway takeoff MTOW 21.5 kg integration80 W power for the from clients. MTOW 21.5 kg key features of the Penguin B innovative1 design. Wonboardide range generator of standard Empty Weight (excl fuel and payload)288mm1 10 kg[11,3in] Wide range of standard Empty Weight (excl fuel and payload) 10 kg subsystemssystem and options AWingvailable Span as an airframe ready for the autopilot3.3 m and payload integration. subsystems and options Wing Span 3300mm3.3 [129,9in]m Length 2.27 m ExtensiveFree Piccolo ® autopilot Length 2.27 m Extensive Wing Area 0.79 m2 documentationconfiguration files set Wing Area 0.79 m2 documentation set Specifications:Powerplant 2.5 hp Powerplant 2.5 hp ShortCatapult, lead car time-top for or Max Payload 10 kg Short lead time for MaxParameter Payload 10Value kg standardrunway takeoff configurations Takeoff method Catapult, Runway or car top launch standard configurations TMTakeofOWf method Catapult,21.5 kg Runway or car top launch Environmental protection 1 Sealed against rain, snow ExtensiveWide rangeDocumentation of standard EnvironmentalEmpty Weight (exclprotection fuel and payload) Sealed10 kg against rain, snow for Penguin B aircraft and 1100mm [43,3in] subsystems and options 1 Wing Span 3.3 m 1 Penguin B with engine and servo package. subsystems. LengthPenguin B with engine and servo package. 2.27 m Extensive 2286mm [90in] Wing Area 0.79 m2 documentation set Performance:Powerplant 2.5 hp Short lead time for ParameterMax Payload V10alue kg Parameter Value standard configurations EnduranceTakeoff method2 20+Catapult, hours Runway or car top launch Endurance2 20+ hours CruiseEnvironmental Speed protection 22Sealed m/s against rain, snow Cruise Speed 22 m/s 901mm [35,5in] 3 1 Stall Speed (with high lift system) 13 m/s StallPengu iSpeedn B with (withengine high and slifterv osystem) package.3 13 m/s Max Level Speed 36 m/s AdvancedUAV Factory fuel Europe injected Max Level Speed 36 m/s Jaunbridagi-1, Marupe, 4 Takeoff run 4 30 m engineLV2167, option Latvia from Performance:Takeoff run 30 m ® CL max (45° flap deflection) 1.7 CurrawongPhone: +371 Engineering 20262126 . CL max (45° flap deflection)163mm [6,4in] 1.7 CL max (clean wing) 1.3 [email protected] 356mm [14in] Parameter Value UAV Factory USA LLC CL max (clean wing) 1.3 UAV Factory USA LLC 2 2 Endurance 1313mm [51,7in] 20+ hours 704mm [27,7in] U5A0V S oFuathc tBourcyk UhoSuAt SLtrLeCet Penguin B with fuel injected engine and 7500cc fuel tank. 50 South Buckhout Street 2 Penguin B with fuel injected engine and 7500cc fuel tank. 5UAV0 So uFactoryth Buc USAkhou LLC.t Street 3 Cruise Speed 22 m/s Irvington, NY 10533 USA 3 Sea level altitude, 15 kg aircraft weight, 15 C°. I50rv iSouthngton Buckhout, NY 105 3Street,3 USA 4 Sea level altitude, 15 kg aircraft weight, 15 C°. Sea level altitude, 15 kg aircraft weight, 153 C°, concrete runway. IrPhone:vington +1, N (914)Y 105 59133 U 3070SA 4 Stall Speed (with high lift system) 13 m/s Phone:Irvington, +1 NY (914) 10533 591 USA 3070 Sea level altitude, 15 kg aircraft weight, 15 C°, concrete runway. Phone:Fax: + +11 ( (914)914) 559191 30703715 Max Level Speed 36 m/s FPhone:ax: + 1+1 (9 (914)14) 5 59191 33296715 [email protected]:e +s1@ (u9a1v4f)a 5c9to1r y3.7c1o5m 4 543mm [21,4in] www.uavfactory.com [email protected] Takeoff run www.uavfactory30 m .com [email protected] www.uavfactory.com CL max (45° flap deflection) 1.7 CL max (clean wing) 1.3 UAV Factory USA LLC Datasheet v 2.0 50 South Buckhout Street 2 Penguin B with fuel injected engine and 7500cc fuel tank. Irvington, NY 10533 USA 3 Sea level altitude, 15 kg aircraft weight, 15 C°. 4 UPhone:NMAN N+1E D(914) PLA 591TFO 3070RMS P SeaE leveNl altituGde, 15U kg aiIrcrNaft we ighBt, 15 C°U, concArete rVunway . PLATFORM AND SUBSYSTEMS Fax: +1 (914) 591 3715 [email protected] www.uavfactory.com Penguin B platform ready for payload and autopilot integration 20+ hour endurance2 Fuel injected engine Penguin's philosophy: option Designed as a high performance unmanned aircraft, Penguin B is capable of up to 26.5 Up to 10 kg payload hour endurance with the 4 kg payload. With a small footprint of 3.3 meter wingspan, capacity Penguin B can handle up to 11.5 kg of combined fuel and payload weight. Modular composite structure, fast assembly, large access hatches, removable payload bay, are the 80 W power from key features of the Penguin B innovative design. onboard generator system Available as an airframe ready for the autopilot and payload integration. Free Piccolo® autopilot configuration files Specifications: Catapult, car-top or Parameter Value runway takeoff MTOW 21.5 kg 1 Wide range of standard Empty Weight (excl fuel and payload) 10 kg subsystems and options Wing Span 3.3 m Length 2.27 m Extensive Wing Area 0.79 m2 documentation set Powerplant 2.5 hp Short lead time for Max Payload 10 kg standard configurations Takeoff method Catapult, Runway or car top launch Environmental protection Sealed against rain, snow 1 Penguin B with engine and servo package. Performance: Parameter Value Endurance2 20+ hours Cruise Speed 22 m/s Stall Speed (with high lift system)3 13 m/s Max Level Speed 36 m/s Takeoff run 4 30 m CL max (45° flap deflection) 1.7 CL max (clean wing) 1.3 UAV Factory USA LLC 50 South Buckhout Street 2 Penguin B with fuel injected engine and 7500cc fuel tank. Irvington, NY 10533 USA 3 Sea level altitude, 15 kg aircraft weight, 15 C°. 4 Phone: +1 (914) 591 3070 Sea level altitude, 15 kg aircraft weight, 15 C°, concrete runway. Fax: +1 (914) 591 3715 [email protected] www.uavfactory.com Datasheet v 2.0 Performance: Sleek and efficient design gives best in class performance. Optimized for endurance, UNMANNED PLATFORMS PPenguinEN has GenoughU internalIN volumeB toU liftA 7.5 Vliters ofP fuelL whichA Twill FprovideO 20+R hoursM AND SUBSYSTEMS endurance with the fuel injected engine.
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