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
Download Presentation The PPT/PDF document " AeroVehicles Inc. 2002" is the property of its rightful owner. Permission is granted to download and print the materials on this web site for personal, non-commercial use only, and to display it on your personal computer provided you do not modify the materials and that you retain all copyright notices contained in the materials. By downloading content from our website, you accept the terms of this agreement.
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