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 AeroVehicles Inc. 2002  AeroVehicles Inc. 2002

 AeroVehicles Inc. 2002 - PowerPoint Presentation

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 AeroVehicles Inc. 2002 - PPT Presentation

Proyectos Aeroespacial Argentinos Nuevas Tecnologías 7 Deciembre 2011 Introduction Definition of a Hybrid Aircraft A hybrid aircraft combines the characteristics of heavierthanair HTA technology fixedwing aircraft or helicopter and lighterthanair LTA airship technology ID: 205367

2002 aerovehicles design aircraft aerovehicles 2002 aircraft design aerocat certificate payload board argentina certification director president type production air

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Slide1

 AeroVehicles Inc. 2002

Proyectos Aeroespacial Argentinos

Nuevas Tecnologías7 Deciembre 2011Slide2

Introduction

Definition of a Hybrid Aircraft

“A hybrid aircraft combines the characteristics of heavier-than-air (HTA) technology, fixed-wing aircraft or helicopter, and lighter-than-air (LTA) airship technology.”AeroCatHas an endurance that can be measured in daysIs capable of landing or taking off with heavy payloads from almost anywhere, including remote fields, deserts, marshes, harbors or waterwaysDevelopment time and cost is a fraction of a comparable traditional new aircraft.The Technology fully developed and safety testedThis is not a new aircraft design, but an updated design using today’s technologyDuring the last seven years, AEROVEHICLES INC. has refined the design and secured the industry partners necessary to certify and produce the AeroCat line of hybrid aircraft. AeroVehicles Inc. 2002Slide3

History

2000

SkyCat

SkyKitten I

1999

1998

Lockheed Martin

AeroCraft

1992

Westinghouse

Sentinel

1000

2006

Lockheed Martin

P-791

2012

AeroCat

AeroVehicles Inc. 2002

AVI VideoSlide4

Benefits of AeroCat

No Ground Infrastructure RequiredLow Capital and Operating CostsEndurance Measured in DaysQuick-change

Payload DeckEnvironmentally FriendlyWeather ToleranceSemi-rigid Design AeroVehicles Inc. 2002Slide5

Specifications

Ancho

Alto: 83 ft / 25.3 mAncho: 148 ft / 45.1 m

Largo:

310 ft / 94.4 m

Allowable useful

load

41,000 kgMaximum payload weight 25,000 kgRange

@ maximum payload ≥ 1200 nmEndurance (varies based on payload) ≥ 36 hrsMaximum efficient cruise speed 70 kts

Nominal

cruise

altitude

1220

mt

Maximum

sustained

altitude

3050

mtEmergency short duration altitude 3660 mt AeroVehicles Inc. 2002Slide6

Alliances

San Luis, Argentina - Facilities

Air Vehicles Ltd., United Kingdom - ACLS TCOM, L.P., United States - Helium Envelope Motive Industries Inc., Canada - Structural Composites INTI, Argentina - Destructive and Non-destructive Testing AeroVehicles Inc. 2002Slide7

FacilitiesZona

Franca Justo Daract; San Luis, Argentina

 AeroVehicles Inc. 2002Slide8

FacilitiesZona Franca Justo Daract; San Luis, Argentina

AeroVehicles Inc. 2002Slide9

Market Analysis

Commercial MarketGeneral

CargoSightseeing/Passenger MarketMineral and Petroleum IndustryHeavy Lift and Oversized CargoCombatting Wild FiresGovernment Agencies:Border PatrolDrug Enforcement Coast Guard Search & RescueDisaster and Humanitarian Aid  AeroVehicles Inc. 2002Slide10

Economic Benefits

Benefits at production rateEstimated 400 new employees inside the FTZ

Additional jobs created to support the FTZProduction revenue over $480 MAncillary revenue not estimated AeroVehicles Inc. 2002Slide11

Competition

Hybrid Air VehiclesTeamed with Northrop GrummanPurchase orders from Discovery

Air Innovations, CanadaFiled for certification with EASALockheed MartinSold production rights to Aviation Capital of CanadaFiled for certification with the FAA AeroVehicles Inc. 2002Spain VideoSlide12

Patents

AeroVehicles Inc. 2002Slide13

Management Team

Chief Executive Officer / Chairman of the Board of Directors:

J. Robert Fort; California, USAChief Operations Officer / President / Director:Bob R. Fowler; San Luis, ArgentinaChief Technical Officer / Board Advisor:Bruce R. Wright; California, USAVice President Business Administration / Director and Board Secretary:M.Sc. Oscar A. Castro Silla; Buenos Aires, Argentina Vice President Operations / Director:Julian Phillip Beville-Anderson; Queensland, AustraliaVice President Legal / Director:Federico Wesselhoefft, LLM (EMLE); Madrid, SpainVice President Information Technology (IT) / Board Advisor:Franco

A. Scillia Thost; Cordoba, ArgentinaDirector of Aircraft Certification DNA / Board

Advisor:Jose Maria

Vaca; Buenos Aires, Argentina Director of Aircraft Certification FAA / Board Advisor:Richard Jensen; California, USA

 AeroVehicles Inc. 2002Slide14

Personnel Plan

75 employees, to design, build and test the first AeroCat SUA.

Approximately 250 employees at full production for AeroCat assemblyAdditional 150 employees for AVI’s alliances in the Zona FrancaMarket value salariesProfit sharing AeroVehicles Inc. 2002Slide15

Schedule

Major

MilestonesPreliminary Design Review (PDR) Month 5Critical Design Review (CDR) Month 10.Hangar Occupancy Month 16 AeroVehicles Inc. 2002Slide16

Certification

Airworthiness Certificate (Aircraft);A standard airworthiness certificate

is the certifying agency's official authorization allowing operation of type certificated aircraft in its stated category.A standard airworthiness certificate remains valid as long as the aircraft meets its approved type design, is in a condition for safe operation and maintenance, preventative maintenance, and alterations are performed in accordance with all applicable regulations Production CertificateA production certificate is an approval (document) to manufacture duplicate products under an approved type design (i.e., type certificate or supplemental type certificate). AeroVehicles Inc. 2002Slide17

Summary

Facts, Not SuppositionsAlliances

Multi-use AircraftProven TechnologyMarket ConfirmedFuture ProductsSecond and third generation products will scale up the capabilities of the AeroCat aircraft to grand proportions: from a 40-50 ton payload to a notional 250-500 ton payload aircraft, capable of transporting time-sensitive cargo trans-oceanic. AeroVehicles Inc. 2002