10.06.2014 MALE TEAM ICARUS FINAL.pptx

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    ICARUS Medium Altitude Long Endurance UAV

    Preliminary Aircraft Design TAU 2!" !

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    Contents!#  Team $rgani%ation

    2#  Time Ta&le'# UAV Re(uirements

    "# Pro)ulsion

    *# System + Payloads Data

    ,# -eometrical De.nition

    /# Structural Layout

    0# Installation Layout

    1# eig3t + 4alance

    !# Aerodynamics

    !!# Performance!2# Conclusions

    !'# A))endi5 A6 Payload info

    !"# A))endi5 4 6 Pro)ulsion

    Preliminary Aircraft Design TAU 2!" 2

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     Team $rgani%ation

    Preliminary Aircraft Design TAU 2!" '

    Eliran 7eger Team Manager

     7anir S3a8ed Eliran 7eger -eometry

    Eyal Tiosano 9i: Snai Structure

    Ar8ady Sitnits8y ;udit3 Eliyani eig3t and 4alance

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     Time Ta&le

    Preliminary Aircraft Design TAU 2!" "

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    MAR=ET SURVE7

    >rom 2!! to 2!/? @orld@ide UAVs mar8ets are )oised toac3ie:e signi.cant gro@t3 as go:ernments @orld@ide mo:e toim)lement more cost eBcient military systems and @ea)onsdeli:ery modalities#

     T3is mar8et @ill gro@ as go:ernments @orld@ide reali%e t3eseaorda&le UAVs can )ro:ide a less e5)ensi:e @ay to )ro:idedefense of a nations &orders and deterrent to intruders#

    In )arallel a signi.cant ci:ilian mar8et starts its de:elo)ment#

    MAR=ETI

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    MAR=ET SURVE7Anot3er factor to aect t3is mar8et gro@ is &asedon t3e creation of ne@ ser:ices eBciencies t3at

    occur from im)ro:ed tec3nologies#

    Additionally? rost + Sulli:an? 20 ;un 2!!

    ,Preliminary Aircraft Design TAU 2!"

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    /

    MAR=ET SURVE7• S)ending for unmanned air :e3icles to dou&le

    o:er ne5t ! years @orld@ide? it3 estimation onMALE mar8et @ill cost a total of !*#* &illion from2!"622'#

      2!' Teal -rou)

    forecast•  T3e UAV mar8et @ill ra)idly gro@ during t3e ne5t

    ! years

      >rost + Sulli:an? 20 ;un 2!!

    DATA 2!*2!"

    Preliminary Aircraft Design TAU 2!"

    http://www.frost.com/sublib/display-market-insight-top.do?id=236443867http://www.frost.com/sublib/display-market-insight-top.do?id=236443867

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    0

    United Ara& Emirates

    MAR=ET SURVE7 6 C$MPETIT$RS

    Preliminary Aircraft Design TAU 2!"

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    1

    MAR=ET SURVE7 6 C$MPETIT$RS

    ISRAEL F EL4IT S7STEMS

    U#S#A F -E

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    !

    MAR=ET SURVE7 6 C$MPETIT$RS

    ISRAEL AER$SPACE I

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    !!

    ICARUS

    An8a Geron TP

    Predator4

    Germes1

     7A4G$uel

     TRACE$E,

     T3ielertCenturion 2#

    !?23) Tur&o

    Pro)

    Rota51!" Tur&o6 "#0 8

    Rota51!" 6!!* 3)

    0!!!*3)

    Po@er

    32,000 '? "*? 2*? '? 2"? Ceilling Hft

    RES$URCEK 2!*2!" 7a&3on 6 smart eye 63tt)K@@@#adcom6systems#comE

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    Ve3icle S)eci.cation

    Preliminary Aircraft Design TAU 2!" !2

    • I F STAR A&ilities• Endurance F "2 H3r

    • ings)an F 2 Hm

    •Lengt3 F ! Hm• Altitude F '2? Hft

    • Range F 2?" H8m

    • eig3t K MT$ F "!'

    H8g

    • Payload F ! H8g

    • >uel F ! H8g

    • 4EMT$ N*O

    • MT$ N 2*O

     

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    Pro)ulsion

    Preliminary Aircraft Design TAU 2!" !'

    3tt)K@@@#traceengines#comengines$E,

    Power to

    Weightratio

    ]HP/![

    "#e

    $o%'(tio%

    [!/h(/h]

     )r*weight

    [kg] Power

    [H(]

    0.5 0.51 130 550 P+A-20

    0.81 0.44 335 600 +RAC .00

    0.9 #"   185 168 A300

    0.69 0.458 64 115 Rota 14 U

    @@@#)@c#ca.lesen=no@yourPT,A#)df 

    @@@#diamondaero#com)roductsDA"2

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    Pro)ulsion

    Preliminary Aircraft Design TAU 2!" !"

     TRACE $E,K

    3tt)K@@@#traceengines#comengines$E,

    as tested as a )otential re)lacement engine on a num&er of aircraft?including t3e Air Tractor ' and " Series Qagricultural? de Ga:illandCanada DGC62 4ea:er and DGC6' $tter Qutility trans)ort? t3e 4eec3craft C1=ing Air Qci:il? Aero Commander * series Qutility trans)ort? and AEAE5)lorer *R Qlig3t multirole# Se:eral ne@ aircraft @ere designed aroundt3e engine as @ell? including t3e TAI 9IU QTur8ey? agricultural and t3e

    Gongdu

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    Preliminary Aircraft Design TAU 2!" !*

    3tt)K@@@#traceengines#comengines$E,

    Pro)eller SelectionAccording toK3tt)K@@@#cul:er)ro)s#comCul:erPro)s#3tml

    E 0'#'O

    A))endi5

    M$DEL AIRPLA

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    Preliminary Aircraft Design TAU 2!" !/

    .

    Chariot& o re !it &*&te'&

    )CoPASS !it &*&te'&

    .R.S IAI

    .SP 3000-H) IAI

    - 1 H) IAI

    W /-212 IAI/-35 IAI

    I""

    +R 400 $a&&i6ia%

    A7/AP8-101 aa'&i

    S+8 15 &a%6ia

    +2000 'i$roair

    Ra6ar978 :e%era Ato'i$&

    /-2055) IAI

      : y6 yPayloads

    A))5# A

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    Preliminary Aircraft Design TAU 2!" !0

    C3osen )ayloadsDecision guidelinesK

    • Pro:en systems• Minimum num&er of su&6contractors• Israeli &ased com)anies

    . W I"" Ra6arChariot& o

    re/)CoPASS

    /-212 +2000 /-2055)

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    ICARUS Con.guration

    Preliminary Aircraft Design TAU 2!" 2

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    -eometrical De.nition

    Preliminary Aircraft Design TAU 2!" 2!

     

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    -eometrical De.nitionCoordinate System

    Preliminary Aircraft Design TAU 2!" 22

     "#/Hm

    Mean Airfoil

    C3ord !#*Hm

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    Side :ie@

    C#-# at 'O M#A#C.

    Preliminary Aircraft Design TAU 2!" 2'

    3eel Diam# A

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    4ottom :ie@

    Preliminary Aircraft Design TAU 2!" 2"

    Lengt3K ! Hm

    S)anK 2 Hm>la)s

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    >ront :ie@

    Preliminary Aircraft Design TAU 2!" 2*

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    Structural Layout

    Preliminary Aircraft Design TAU 2!" 2,

    • Aerodynamic structure• Smoot3 lines•

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    Structural Layout

    RESOURCE:

    http://www.christinedemerchant.com/carbon-kevlar-glass-comparison.html

    http://www.corecomposites.com/composites/reinforcements

    Preliminary Aircraft Design TAU 2!" 2/

    Car!o% !er& 3a:e t3e3ig3est rigidity of allcommercial a:aila&le .&ers#

     T3ey oer high $o'(re&&i;ea%6 te%&ie &tre%gth?dura&ility for corrosion? cree)and fatigue#

    -ga&& is anot3er ty)e of .&ercontaining 3ig3 condensed

    numerous e5tremely .ne glass.&ers# T3ey oer &ad fatigueresistance and @ill (uic8lyloose t3eir a&ilities#

    ighter (art& can &emanufactured using car&on

    .&ers t3en @it3 E6glass#Moreo:er? less .&ers areneeded @3en using car&on.&ers in order to reac3 t3esame :alue of strengt3 andrigidity#

    http://www.christinedemerchant.com/carbon-kevlar-glass-comparison.htmlhttp://www.christinedemerchant.com/carbon-kevlar-glass-comparison.htmlhttp://www.corecomposites.com/composites/reinforcements/http://www.christinedemerchant.com/carbon-kevlar-glass-comparison.htmlhttp://www.christinedemerchant.com/carbon-kevlar-glass-comparison.htmlhttp://www.corecomposites.com/composites/reinforcements/http://www.corecomposites.com/composites/reinforcements/http://www.corecomposites.com/composites/reinforcements/http://www.christinedemerchant.com/carbon-kevlar-glass-comparison.htmlhttp://www.christinedemerchant.com/carbon-kevlar-glass-comparison.html

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    Installation Layout

    Preliminary Aircraft Design TAU 2!" 20

    Landing-ear Landing -ear Co:ers

    E$RADAR

    I>>

    E

    Engine>UEL

    RA)AR ELM2**

    . QC3ariot of >ire DCoMPASS

    I"" T2

    W ELL02!2

    >uel Tan8

    Pro)ulsion

    A;io%i$&

    AVI

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    '

    eig3t + 4alance

    Weight (kg) Distance from nose (m)

    Fuselage !".# $.%

    wing &$$$.' '.&

    Tail- Horizontal &(.! %.'

    Tail- Vertical (% %.'

    Propulsion $$' %.$

    EO Chariot of Fire (" &.'  DCoMPASS $# &.'

    EW ELL8212 &"" '.'IFF 2!!! ".* !."

    RADAR ELM2!"" (" &.#

    Fuel &""" '.&

    MTOW 3893#ensit$ gm%cm&' a thickness *mm+ Distance from the attack of the ing *m+ aero#$namics string *m+

    car,on &.(&!. *. &.'

    E-gass &.%

     A(m&2) Weight (kg)

    F.eseage $!.*$ !".#

    ing (" &$$$.'

    ai- /ori0onta .%$ &(.!

    ai- ertica $ (%

    Pro.sion $$'

    BEWPropulsion 2635

    Pa!loa"s 258

    Fuel 1000

     BEW-#MA$ 30.6

    MTOW - #MA$ 28.2

    "#/Hm

    M#A#C#!#*Hm

    ∗nose

    Preliminary Aircraft Design TAU 2!"

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    Aerodynamics

    Preliminary Aircraft Design TAU 2!" '!

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    Aerodynamics

    Preliminary Aircraft Design TAU 2!" '2

    62 6!* 6! 6* * ! !* 2 2*

    62

    6!

    !

    2

    '

    "CL Vs# al)3a

    al)3a HdegI

    CL HI

    62 6!* 6! 6* * ! !* 2 2*

    #*

    #!

    #!*

    #2

    #2*

    #'

    #'*

    #"CD Vs# al)3a

    al)3a HdegI

    CD HI

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    Performance

    Preliminary Aircraft Design TAU 2!" ''

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    Performance

    Preliminary Aircraft Design TAU 2!" '"

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    Performance

    Preliminary Aircraft Design TAU

    2!" '*

     9a!ho%

    I$ar#&

    Hero%+P

    Her'e&

    Pre6ator>

    A%k a

    &!" *! $( $( $' !* EnduranceH3rs

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    Performance

    Preliminary Aircraft Design TAU 2!" ',

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    Performance

    Preliminary Aircraft Design TAU 2!" '/

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    Performance

    Preliminary Aircraft Design TAU 2!" '0

    • Ma5 Altitude F '0 8ft• Ma5 R$CF !'* ftmin• Endurance F "2 3r• Ma5 Range F 2" 8m• CLma5 F 2#,• LD ma5 F !1#*

    • Ma5 Ta8eo Distance Q3* ft F 1*m• Ma5 Landing Distance Q3* ft F

    !/ m

    • Ma5 Velocity F !* 8ts

    SummaryK

     Ta8eo -round Roll

     Ta8eoDistance

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    Conclusions

    Preliminary Aircraft Design TAU 2!" '1

    • Gig3 Performance MALE UAV

    • Long o)erating distance for ad:ancedISR ca)a&ilities

    • State of t3e art )ayload for :ariedmissions

    • Gig3est Endurance + Altitude at itsclass

    Manufacturing

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    A))endices

    Preliminary Aircraft Design TAU 2!" "

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    A))endi5 A6 Payloads info

    E$EI>>RADAR

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    C3ariots of >ireAutonomous Air&orne Gy)ers)ectral MASI

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    )CoPASS?Digital Com)act Multi6)ur)ose Ad:anced

    Sta&ili%ed System 6 Air&orne

    3tt)Kel&itsystems#comEl&itmain.lesDCoMPASSO2AirQne@#)df  2**2!"

    http://elbitsystems.com/Elbitmain/files/DCoMPASS%20Air(new).pdfhttp://elbitsystems.com/Elbitmain/files/DCoMPASS%20Air(new).pdfhttp://elbitsystems.com/Elbitmain/files/DCoMPASS%20Air(new).pdfhttp://elbitsystems.com/Elbitmain/files/DCoMPASS%20Air(new).pdf

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    L$R$SL$ng Range $&ser:ation System

    3tt)K@@@#iai#co#il2!'!0,006'/*6enSystemMissileandS)aceTamamElectro

    http://www.iai.co.il/2013/18688-30075-en/SystemMissileandSpace_Tamam_Electro-Optical.aspxhttp://www.iai.co.il/2013/18688-30075-en/SystemMissileandSpace_Tamam_Electro-Optical.aspxhttp://www.iai.co.il/2013/18688-30075-en/SystemMissileandSpace_Tamam_Electro-Optical.aspxhttp://www.iai.co.il/2013/18688-30075-en/SystemMissileandSpace_Tamam_Electro-Optical.aspx

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    M$SP '6GD Tamams GD Multi6sensor $)tronic Sta&illi%ed Payload

    3tt)K@@@#iai#co#il2!'!0,006!,,,/6enSystemMissileandS)aceTamamElectro

    http://www.iai.co.il/2013/18688-16667-en/SystemMissileandSpace_Tamam_Electro-Optical.aspxhttp://www.iai.co.il/2013/18688-16667-en/SystemMissileandSpace_Tamam_Electro-Optical.aspxhttp://www.iai.co.il/2013/18688-16667-en/SystemMissileandSpace_Tamam_Electro-Optical.aspxhttp://www.iai.co.il/2013/18688-16667-en/SystemMissileandSpace_Tamam_Electro-Optical.aspxhttp://www.iai.co.il/2013/18688-16667-en/SystemMissileandSpace_Tamam_Electro-Optical.aspx

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    M6 !1 GDLong Range GD Multi6sensor $&ser:ation and Targeting

    Pay8oad

    3tt)K@@@#iai#co#il2!'!0,006"*'1'6enIAI#as)5  2**2!"

    http://www.iai.co.il/2013/18688-45393-en/IAI.aspxhttp://www.iai.co.il/2013/18688-45393-en/IAI.aspxhttp://www.iai.co.il/2013/18688-45393-en/IAI.aspxhttp://www.iai.co.il/2013/18688-45393-en/IAI.aspx

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    E

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    3tt)K@@@#iai#co#ilsi)storage>ILES',0'#)df  

    ELL602!2

    ELL 0'0*

    http://www.iai.co.il/sip_storage/FILES/0/36830.pdfhttp://www.iai.co.il/sip_storage/FILES/0/36830.pdfhttp://www.iai.co.il/sip_storage/FILES/0/36830.pdfhttp://www.iai.co.il/sip_storage/FILES/0/36830.pdf

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    3tt)K@@@#iai#co#il2!''""0,62,"116enIAI#as)5  2* * 2!"

    ELL60'0*

    http://www.iai.co.il/2013/34486-26499-en/IAI.aspxhttp://www.iai.co.il/2013/34486-26499-en/IAI.aspxhttp://www.iai.co.il/2013/34486-26499-en/IAI.aspxhttp://www.iai.co.il/2013/34486-26499-en/IAI.aspx

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    I>>

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    LTR "

     

    3tt)K@@@#cassi dian#com@e&guestltr6"2* * 2!"

    A> Trans)onder

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    A> Trans)onder

     

    3tt)K@@@# #comProductsElectronicsI>>SystemsI>>Systems#3tml

    http://www/http://www/

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    STW !,* Trans)onder

     

    3tt)K@@@#sandia#aero(node,, 2* * 2!"

    http://www.sandia.aero/?q=node/66http://www.sandia.aero/?q=node/66http://www.sandia.aero/?q=node/66http://www.sandia.aero/?q=node/66

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    Radar

    L7

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    L7

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    ELM62**

     

    3tt)K@@@#iai#co#ilsi)storage>ILES*',0'*#)df  2**2!"

    http://www.iai.co.il/sip_storage/FILES/5/36835.pdfhttp://www.iai.co.il/sip_storage/FILES/5/36835.pdfhttp://www.iai.co.il/sip_storage/FILES/5/36835.pdfhttp://www.iai.co.il/sip_storage/FILES/5/36835.pdf

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    Preliminary Aircraft Design *1

    A))endi5 46 Pro)ulsion

     T3rust CoeBcientPo@er CoeBcient

     

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    Pro)ulsion !

    Pro)eller EBciency

    V !'2 ftsec 1MPG

    n '* re:sec 2*,RPMD /#* ft 1 inc3

     T3ereforeK

    AndK

     

    M$DEL AIRPLA

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    >igure !

    Pro)ulsion 2

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    Pro)ulsion '

    >igure 2