presentacion nostromo panama
TRANSCRIPT
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PRESENTACION : NOSTROMO DEFENSA S.A
UAV Tcticos para Misiones ISTAR
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Presencia y Cooperacin Global
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INFANTERIA DE MARINA ARGENTINA
ANFIBIO IIAGOSTO2009
PATRIAE SEMPER VIGILES
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ANFIBIO II
AGOSTO2009
CHECK POINT FUERZAOPOSITORA
Misin Tpica EO -CCD x Zoom ptico x 10-Estabilizada
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BATALLON COMUNICACIONES EINTELIGENCIA
EJERCITO PARAGUAY
CABURE UAV
Operado 100 % por personal Paraguayo
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UAV TACTICO PROPULSADO POR MOTORES WANKEL A INYECCION
ELECTRONICA -COMBUSTIBLE PESADO (JP-8)
VINGBIRD UNMANNED AERIAL SYSTEM
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DEFINICION CONCEPTUAL DE UAV TACTICOS EN MISIONES ISTAR
REQUERIMIENTOS OPERACIONALES TIPICOS
Current requirements for mobile forces require intermediate range ISRmissions (minimum 30 km ) from land and sea .
Other forces requirements push for rapid deployment of UAV system inthe battlefield by helicopters, cargo aircraft ,small craft or light groundvehicles Quiet , fast reaction UAV systems are needed for day/night operations
with limited human resources Quick deployment and post deployment are essential to mobile forces Persistent Surveillance requires long endurance and high reliability ofcomponents (4 hours minimum ) Easy to operate and compact ground control station is also a need for
forces deployed with minimum resources
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Concept DefinitionTypical Operational Requirements II
Integration with land observation systemsand battle managment system is mandatory
Low acoustic signature as well as IR andRadar signatures are mandatory to keep theoperative force undetected
Weight of the overall system ( UAVs ,
Container-Launcher, GCS ) shall be less than50 kg
Rugged UAV and rugged system are specificrequirements for forces that are operating inharsh environments .
UAV shall be able to perform a high rate ofclimb, sustain several operation modes, havelong endurance, be able to sustain veryquiet operation mode , be airborne in veryshort time with minimum preparation
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MAINTYPICALMISSIONS ISTAR(INTELLIGENCESURVEILLANCETARGETADQUISITION
RECONNAISSANCE)
BDA(BATTLE
DAMAGE
ASSESSMENT
)
EW/IW(ELECTRONICWARFAREINFORMATIONWARFARE)
NBCMONITORING
GEOSPATIALINTELLIGENCE
PERSISTENT SURVEILLANCE(BORDER
PATROL
,HOMELAND
SECURITY)
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SOURCE:
TheEmergence
of
Mini
UAVs for
Military
Applications
byTimothyCoffeyandJohnA.MontgomeryDEFENSEHORIZONS
TECHNOLOGYMATRIXFOR MINIUAVPAYLOADS
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EVOLUTIONOF SMALLUAVCONCEPTS
MISSIONFOCUSEDCONFIGURATIONDESIGN
ENGINETECHNOLOGY
EVOLUTION
IS
A
PRIORITY
TO
EVOLVE
IN
UAV
CAPABILITIES
AND
OPERATIONALFLEXIBILITY
Scan Eagle
Inflexion Point
Vingbird
New Concept
Toomany UAVto
accomplishment the
Mission Matrix
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VINGBIRD
LONG ENDURANCEHIGH PERFORMANCES
FLEXIBLE OPERATIBILITY
AN ADVANCED AIRFRAME CONCEPT DESIGNED AROUND A HIGH TECHNOLOGYROTARY INJECTION ENGINE RUNNING IN HEAVY FUEL
UNSURPASSED IN ITS CLASS
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NOSTROMO-CUBEWANO YARARA UAV WANKEL INJECTION ENGINEPOWERED BY MOGAS/HEAVY FUEL
VINGBIRD TECHNOLOGY BACKGROUND
MANTIS -NOSTROMO DEVELOPMENT FOR A THIRD PARTY
VINGBIRD INTEGRATED AIRFRAME CONCEPT AROUND A HIGH-TECH ENGINE
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YARARA UAV WITH CUBEWANO WANKEL INJECTION ENGINE
POWERED BY MOGASDECEMBER 2008
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YARARA UAV WITH CUBEWANO WANKEL INJECTION ENGINE
POWERED BY MOGASDECEMBER 2008
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YARARA +SONIC 35 WANKEL HEAVY FUEL
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Launched by handTwin
Electrical
Engine
2 Hs1 Kg1 HP8.2 KgDRAC -EADS
Electrical
Engine
2 Hs1.1 Kg1 HP5.5 KgSkylark Elbit
Electrical
Engine
1.5 Hs1.2 Kg0.8 HP6 kgOrbiter
Aeronautics
-ElectricalEngine
2 Hs1 Kg1 HP6 KgAerovironmentPuma
US SOF developmetElectric
Engine
2 Hs1 Kg1.2 HP6.5Lockheed Martin
Stalker
Heavy fuel in
development
4 Stroke
engine
8 to 10 Hs1.5 Kg|1.8 HP12 kgSilver Fox-ACR
Modified 2 stroke
engine for heavy fuel in
development
derivation of 3W Model
Aircraft Engine
2 stroke gas
engine
15 to 20 hs
depending of
payload
2-3 kg1.9 HP18 kgScan Eagle
Boeing
RemarksnginetypeEnduranceayloadowerTOWystem
STATE OF THE ART :MINI UAV MEDIUM/LONG ENDURANCE CAPABILITY
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STATE OF THE ART :MINI UAV MEDIUM/LONG ENDURANCE CAPABILITY
Issues : Electrical powered UAV will not reach long endurance due battery energy density. ,so
persistent surveillance is not possible with power system. Fuel cell technology in theforeseeable future will extend the endurance but limited to 4 to 6 hours with limitedextra electrical power on-board
Current players powered by internal combustion engines ,are using either modifiedengines from model aircraft or small machines manufacturers .So realibility andairworthiness is an unresolved issue
Multi -fuel engines with injection system are not used by current players
Injection system with electronic control to get automatic altitude compensation is notused by current players
Advanced airframes and aerodynamic concept elaborated around a high technology
engine has not been the case in the UAV industry Minimum requirements for launch and recovery as well as operation has not been the
standard for the current systems in use.
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System Main Design Goals
Engine Integration Wing Design Fuel System Sensor integration Operational Flexibility
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Design Innovation :
Fully Integrated Airframe
around the engine
Wing design : flaps andailerons with positive and
negative deflections adapting
the wing lift to minimize drag
and flight regimes flexibility
Catapult Launched for
extreme endurance and
capability of hand launch for
limited endurance
Recovery at minimum weight
using deep stall technique and
airbag
Minimum weight at landing is
achieved by expeling remain
fuel in the tank
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VINGBIRDCUTAWAY
Nose Details
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Flaps down for take off/landing/low speed
manuever
Negative Ailerons
deflections at high speed
/or low wing loading to
minimize trim drag
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Performances At H= 3000 mts
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Performances At Sea Level
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ENDURANCEVS PAYLOADFORTWODIFFERENTMTOW
27 MTOW:MAXIMUMTAKEOFFWEIGHT
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ElectricalPowerGenerationOnBoard
28
The Sonic 10 has an electrical generator that
delivers 200 Watts of power at cruise RPM
and500WattsatmaximumRPM
135,0TOTAL10,0Actuators
2,5Electrical system
2,5Avionics
120,0Engine auxiliaries (oil pump,
fuel pump, ECU, ignition coils,injector, etc)
Power [Watts]Elements
Power consumption at cruise
5,0Data link
5,0PSAR
20,0EO/IR sensor
5,0Video TX (Range: 50 km)
Power [Watts]PayloadExamples of payloads power consumption
At cruise the Vingbird can deliver 65 Watts
of electrical power for payloads.
The Vingbird electrical power generation onboard
allowstofulfillthedemandofhighpowerpayloads.
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CUBEWANO SONIC 10 : 2HP- HEAVY FUEL REDUCTION DRIVE
VINGBIRD ENGINE
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DesignAir Cooled
High power to weight ratio
Low Vibration
Lightweight constructionSeparate oil system
Electronic engine management
Extensive use of high tech materials.
Flexible Power possibilities from 2 to 7.5hp
with simple design alterations
INJECTION ROTARY ENGINE TECHNOLOGY
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Specification(2hp)
Sonic 10
Proposedlayout(shownwithgenerator)
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SONIC 10 LAYOUT
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ModularSeamlessPayloadSystem
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VINGBIRD
COMPLETE SYSTEM
2 TRANSPORT CASES +GCS+2 UAV
VINGBIRDSTANDALONEDEPLOYMENT
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VINGBIRD
TRANSPORT CASE 2 UAV
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Vingtaqs II -SIMRAD OPTRONICS
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Vingtaqs II -SIMRAD OPTRONICSLong range, target acquisition and surveillance system / forward observer
system.
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VINGBIRDINTEGRATEDINVINGTAQSII
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VINGTAQSIILAUNCHINGAVINGBIRD
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VINGTAQSII+VINGBIRDEXTENDEDSITUATIONALAWARENESSSYSTEM
EO/IRISTAR
MISSION
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VINGTAQSII+VINGBIRDEXTENDEDSITUATIONALAWARENESSSYSTEM
TARGETDESIGNATIONMISSION
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VINGTAQSII+VINGBIRDEXTENDEDSITUATIONALAWARENESSSYSTEM
ELECTRONICWARFAREMISSION
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VINGTAQSII+VINGBIRDEXTENDEDSITUATIONALAWARENESSSYSTEM
BATTLEDAMAGE
ASSESSMENT
(BDA)
MISSION
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Small Tactical UAV Caburei
Lateral Gyrostabilized EO - Sensor
A Low Cost Solution for Small Tactical ElectricalPowered UAV to Improve EO Sensor Capabilities
Small UAVs State of the Art
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Small UAVs State of the Art
Most of the small UAV in the tactical battlefield with weights under 4 Kilograms are onlyequipped with fixed frontal and lateral EO sensors. These sensors packages have strong
limitations to use zoom and usually the flight altitude is very low in order to engage
targets in the ground .
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C G O 1
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CLGE -EO MK1
Lateral Gyro Stabilized Payload for Small
Tactical Electrical Powered UAV
Interchangeable Sensor : EO Daylight with
optical zoom or IR camera with digital zoom
Developed by FixView -Cordoba -Argentina
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Caburei flying with CLGE
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GRACIAS POR SUATENCION