Presentacion Nostromo PANAMA

8/14/2019 Presentacion Nostromo PANAMA

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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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TARGETDESIGNATIONMISSION


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ELECTRONICWARFAREMISSION


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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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