ࡱ> qp =\6 John Pike [B=Sheet1$ ; P#=%8X@"1Arial1Arial1Arial1Arial1Arial1Arial1Arial1Arial1Arial1Arial1Arial1Arial1Arial1%Arial1Arial1@Arial1@Arial1@Arial14Arial1hArial"$"#,##0_);\("$"#,##0\)"$"#,##0_);[Red]\("$"#,##0\) "$"#,##0.00_);\("$"#,##0.00\)%""$"#,##0.00_);[Red]\("$"#,##0.00\)5*2_("$"* #,##0_);_("$"* \(#,##0\);_("$"* "-"_);_(@_),))_(* #,##0_);_(* \(#,##0\);_(* "-"_);_(@_)=,:_("$"* #,##0.00_);_("$"* \(#,##0.00\);_("$"* "-"??_);_(@_)4+1_(* #,##0.00_);_(* \(#,##0.00\);_(* "-"??_);_(@_)                + ) , *      @        ( @ ` r h Mr@  h H@  `     ` r  `    ( @ ` @ @  ` r@  ` @  ` r@ "8   (0 @(0 (x @)x I@ (x I@ (x I@ (x AsI@  (8 @ (8  *x r@ *x @ (x Q@  (x A  (x A (x I@  )x I@  (x I@  (x Q@  (x Q@  (x A  (x A  (x Q@  (x A  *x Mr@  *x H@ *x Mr@ (x H@  h r    x r@8 @(x A  (x A  )x AI@  (x I@ (x A  *x AI@ *x AI@  *x I@  *| @  *| Q@  *| A (P (P  *x AI@  *x I@  *| @  *| Q@  *| A  *x @I@  (8 I@  *x I@  *| @  *| Q@  *| A (X (x AI@ *x AI@ (P (x AI@  *x I@  *x I@  *x AsI@  *x AsI@  *| As@  *| AsQ@  *| AsA (p As ( *0  *8  *< @  *< @ *<  *< (x Mr@ *p r *x r *| r@  *| r@ *| r *| r  (x r*p  *x  *| @  *| @ *|  *|   (x  *x AI@  *x A  (X  *x AI@  *x A  (x I@  *x AI@  *x AI@ ( )x I@  )x I@  )x  (X  )x A  (x I@  (x AI@    (  )8 @ (8   (  @   @  h mr@  ` Es  h h@  ` @  *x Ai@  *| A  *x Ai@  *| A  *x @i@  *| A (x Ai@ (x Ai@ (x i@ (x i@ (x Asi@  *| AsA  (8 (@ *< @ (x mr@  *| Es (x h@  *| @  *x Ai@  *x Ai@  *x Ai@  *x Ai@  *x Ai@  *x AI@  (x AQ@ (x AA  *x AA  *| A@  *| AQ@  *| AA  *| AA  : H@ (: H@   : H@   ( M@   ( M@  M@  M@  x r H@   ( H@  (x AI@  ( -@ ( (@ H@  ( (@8 (@ : H@  Sheet1 = ^!Cv  dMbP?_*+%&C&DMHP LaserJet 4M Plus@g XX@MSUDNHP LaserJet 4M Plus;d "dXX??U} } A} Q}  } } } } Column Z ^$$b$\$\Z$\b$\$hZ $h $h@ڱ $  $ځ $b $b$h$\$e@ $hP$\@$PV$Pf$\V$\W$\c$bf$\V$f$\V$f$V$f$VGRevisionH`r@2A *      )Overall Payoff # Key . &FWV Technology Demonstrator Weightings f ???D@>@>@T@?4@?4@>@4@>@??         FWV Goals #9 .9 Positive/Improvement/>150lb Weight Reduction   H +,%#%# #9 .9 Positive/Improvement/>150lb Weight ReductionL +,# 3 Neutral/No ChangeL +,#6 +1 Negative/Decrement/>150lb Weight IncreaseL +,#H=FWV Demonstrator Totals = Sum(Attributes X Weighting Factors)L+,#bWFWV Tech Demo (Goal Weighted) = Sum(Attributes X Weighting Factors) X COF X Goal Totals L+,#zoBaseline for Comparison: Unmanned Vehicle with F-22 or F/A-18E/F 1995 Technologies, UAV Ground Control Station   J ,#Technology Timeframe (2000) Acquisition Cost O&S Cost Mission Radius Low Alpha S&C High Alpha S&C Sustained "G"!Configuration IntegrationPayloadFlight ControlsMission SensorsSupportability Survivability UCAV Enabler,$Prioity to Government and ContractorMass PropertiesFWV Demonstrator Totals$Consequence of Failure (COF)IA Next Demonstration (A=Analytical, G=Ground Test, F=Flight Test)Total with COF' Reduced Production Cost at T1 Reduced O&S Costs Reduced EMD Cost! Reduced Airframe Weight  Improved Cruise L/D*!" Improved Agility/Maneuverability" Goal Totals'#FWV Demonstrtor (Goal Weighted)WL/FIBWL/FIMWL/FIGWL/FIVWL/XPNLockheed*I" Technologies and Technology Sets D DescriptionF Attributes&(&( !!!# Structures Aeromechanics Flt Controls SubsystemsMartinB-E'$'$""# X PXP PXQ PX>06Compact Inlet System / Inlet-aerostructure integrationY;QCompact, Fixed Geometry Inlet System for Reductions in Aircraft Volume and WeightfR"@R"@R"@R"@R@R@R@R"@R@R@R@R@R"@R@R"@R"@SffffffQ@L @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @L~ T"@ SFT33333@#- LL UX UX UX UX U !UX~ "S@#x@(### LL X XXX XX XX XXogExhaust system: low-cost yaw vectoring, plume mixing/shape, structural integration, fluidic/fixed area)yFixed Nozzle Geometry, Elimination of Moving Parts. Fluidic Control Adjusts Nozzle Flow Area and Enables Thrust VectoringfY"@Y"@Y"@Y?Y"@Y"@Y"@Y"@Y@Y@Y@Y"@Y"@Y@Y"@Y"@Zfffff&S@+L @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @L~ [@ ZG@# \X \X \X \X \ !\X~ "Z@#@*### LL P PXP PX PX%0UAV/UCAV Control (Data Links)B0:Spoof-Proof, Secure, Anti-Jam, Stealth, Variable BandwidthfR"@R?R@R@R@R@R@R?R@R@R@R?R"@R"@R"@R@S433333D@~ T"@ SATv@# UXU UXU  UX !UX~ "S@#@E#### LL ]X ]X] ]X ]X/TaillessO^GNo Vertical or Horizontal Tails for Low Drag and Excellent LO Qualitiesf_"@_@_@_@_@_?_@_@_@_@_@_@_"@_@_"@_"@`LH@~ a@ `Fa23333Cu@# bX bb bX  bX!b~ "`@#@### LL P PXP PX PX30+UAV / UCAV Control (Close Formation Flight)B0:Enables Cooperative Flight Operations of Multiple AircraftfR?R?R"@R"@R?R@R@R?R@R@R?R?R"@R@R"@R?SB@~ T"@ SAT@t@#U UX UU  UX !UX~ "S@#`@### LL X XX XXX XX XXK9CAdvanced Wing Platforms: Continuous/conformable moldline technologyxStructurally Sound Memory Elastic Material with Application to Expandable Fuel Tanks and Weapons Bays, Control Surfaces.fY"@Y@Y@Y@Y"@Y"@Y"@Y@Y@Y@Y@Y@Y"@Y@Y"@Y@ZI@~ ["@ ZFffff}@#\\\\  \X !\X~ "Z@#fffff@### LL PX PPQ PX,0$Advanced Wing Platforms: Lambda Wing7/Planform Shape That Offers Aerodynamic BenefitsfR"@R?R@R@R@R@R@R@R@R@R@R@R"@R@R"@R?SC@~ T@ SFTh@# UUU UX  UX !UX~ "S@#`@### LL X XXX XX XXB:Composite Structures (Low cost, lightweight, limited-life)Use Large Unitized Structural Composite Parts to Minimize Hand Labor, Part and Fastener Count. Relaxed Structural Criteria for Limited Life.fY"@Y"@Y"@Y"@Y@Y"@Y@Y@Y@Y@Y@Y@Y@Y@Y@Y"@ZM@D @DD @ D D @ D D @ D D @ D D @ D D @DD @DD @DD @DD @DD @DD @DD @DD @DD @D~ [@ ZG@# \X \X\ \X  \\!~ "Z@#gffff^@@# DD" P PXP PX PX.0&UAV/UCAV Control (Single Ship Control)=05Emphasis of Automated Guidance and Control AlgorithmsfR"@R?R"@R@R@R@R@R@R@R"@R@R@R"@R"@R"@R@SK@~ T"@ SAT~@#UUUUU  !UX~ "S?#~@# X XX Xe XX79/Multivariable control/effectors: reconfigurablephControl Law Design Algortithms which Execute On-Line and Real-Time to Yield Maximum Possible PerformancefY"@Y@Y"@Y"@Y"@Y"@Y"@Y"@Y@Y@Y@Y"@Y"@Y@Y"@Y@Z43333P@~ [@ ZFi@# \\ \X \\  !\X~ "Z@#ly@$### LL XQ PXQ PX PX5.-Active aeroelastic wing/twist wing technology:}Use Aeroelastic Flexibility with Leading and Trailing Edge Devices. Twist Wing With Torque Tube To Generate Roll (No Aileron)fR"@R?R@R"@R@R@R"@R?R@R?R@R?R@R@R"@R@SLE@~ T@ SFT43333_@# UUU UX  UX !UX~ "S@#gffffw@+### LL X XXX XX XX59-Power-by-wire/fly-by-light/electric actuationXPReplacing Many or All Hydraulic and Mechanical Systems Associated With ActuatorsfY"@Y@Y@Y@Y@Y@Y@Y@Y@Y@Y@Y"@Y"@Y@Y"@Y"@ZI@~ [@ ZF[ c@#\ \X\ \X  \\!~ "Z@# s@### LL PX PX PQ PX,0$Flow Control: MEMS (flow separation)x;pMicromechanical Devices for Viscous Drag Reduction, Control Effectors, Active BL Control and Vortex ManipulationfR?R@R?R"@R@R"@R"@R@R@R@R?R@R"@R@R"@R"@SfffffG@~ T@ SATa@#UUUU  UX !UX~ "S@#q@### LL@+D O55]1r=BQ"H $\bf!$V"$Zf#$\V$$\f%$\ZV&$\f'$V($f)$V*$bf+$\V,$\f-$\V.$f/$\V@0$ f@1$PV2$\Pf3$ho 4$hp5$hp6$hb~7$\8$9$\:$;$\f<$\V=$f>$V?$f ggg XX XX6 9.Laminar flow control for low aspect ratio wing: 92Active Flow Enhancement for Low Aspect Ratio Wingsf Y"@Y?Y?Y"@Y@Y@Y@Y?Y@Y@Y@Y?Y@Y@Y@Y? Z=@   -L @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @L~ [@ ZG V@ # \\\ \X \X !\~ "Z@ #Yf@' # ## LL !PP !PX!Q !PXH!0@Light-weight landing gear: graphite epoxy/titanium metal matrix?!07New Material Applications to Reduce Landing Gear Weightf!R"@R?R"@R"@R@R@R@R@R@R@R@R"@R@R@R"@R"@!SL@! ~ !T@ !SG!T43333e@!# !UU !U  !UX ! UU!~ !"S?!#43333e@-!#!!## LL "XX "XX"e "eX9"91Structurally-integrated thermal energy managementd"9\Optimized Solution for Both Subsystems and Structural Cooling in an Exhaust Washed Componentf"Y"@Y"@Y"@Y?Y@Y@Y@Y"@Y@Y@Y@Y"@Y"@Y@Y"@Y"@"Z Q@"~ "[? "ZG"[ Q@"#"\ "\X "\  "\X " \\!~ ""Z@"# a@"#""## LL #P #PX#P #PX #PX-#0%UAV/UCAV Control (Multi-Ship Control)0#0(Single Control Station, Muliple Vehiclesf#R"@R"@R"@R@R@R@R@R?R@R"@R@R?R@R@R"@R@#S33333L@#~ #T? #SA#T33333L@###UUUU # UX #!UX~ #"S@##33333\@#$ $XX $XX $XeX-$9%Flow Control: Forebody vortex control6$.Mechanical Device Used for Vortex Manipulationf$Y"@Y@Y?Y@Y@Y"@Y@Y?Y@Y@Y@Y@Y?Y@Y@Y?$Zgfffff?@$~ $[@ $ZG$[̌W@$#$\\\\\  $!\X~ $"Z?$#̌W@$#$$## LL %PP %PX%Q %QX0%0(Light-weight HX: carbon-carbon composite5%0-High Temperature, Light Weight Heat Exchangerf%R"@R?R?R"@R@R@R@R@R@R@R@R?R@R@R"@R"@%SfffffF@% ~ %T? %SG%TfffffF@%#%U %UX%U %UX % UU!~ %"S@%#fffffV@"%#%%## LL &XX &XX&e &XX,&9$Light-weight HX: EHD heat exchangers5&9-High Temperature, Light Weight Heat Exchangerf&Y"@Y?Y?Y"@Y@Y@Y@Y@Y@Y@Y@Y?Y@Y@Y"@Y"@&ZfffffF@& ~ &[? &ZG&ffffF@&#&\ &\X&\ &\X & \\!~ &"Z@&#fffffV@%&#&&## LL 'd 'PX'd 'PX 'PX1'0)Affordable, LO Air Data System (optical?)h'0`Measures Critical Air Mass Flow Properties Based on Aerosol Particle Structure of the Atmospheref'R"@R"@R@R@R@R@R@R@R@R@R@R@R"@R"@R"@R@'SI@' ~ 'T? 'SF'TI@'#'UUUUU  '!UX~ '"S?'#I@!'#''## LL( (XX (XXe (X Z(9RIntegrated weapons carriage: Internal carriage load reduction (including acoustic)f(^Aero Interaction Aspects of Separation and Load Eleviation Using Active or Passive Suppressionf(Y"@Y?Y@Y@Y@Y@Y@Y@Y"@Y@Y@Y@Y@Y@Y@Y@(ZA@(~ ([? (ZG(@(#(\ (\X(\\\\!~ ("Z?(#A@)(#((## LL) )PX )PPQ )PX:)02Integrated weapons carriage: External weapons podsT);LAlternate to Internal Weapons Carriage in a Signature Controlled Environmentf)R"@R?R?R@R@R@R?R?R?R@R@R?R"@R@R"@R?)SL@@)~ )T? )SF)TL@@)# )UUU )UX ) UU!~ )"S?)#L@@)#))## LL *X *XX *XX *ee*Decoupled fuel cellsZ*RConfineable Fuel Tanks to Reduce Vulnerability to Ballistically Impacted Munitionsf*Y"@Y?Y?Y?Y@Y@Y@Y"@Y@Y@Y@Y?Y"@Y@Y@Y?*ZgffffA@*~ *[? *ZG*ffffA@*#*\\\\\\!~ *"Z*# D*"D* +X +PPP +P? +PX/+.'Conformal loadbearing antenna structure5+:-Enables Use of Large Multi-Function Aperturesf+R"@R?R?R@R@R@R@R"@R@R@R@R?R"@R@R@R@+SLC@+~ +T? +SG+TLC@+#+UUUUUU!~ +"S+#+#++## LL ,XX ,XX,e ,XX:,92Fire suppression: fuel tank and engine compartmentE,9=Halon 1301 Replacement for Inerting Tank and Bay Compartmentsf,Y"@Y?Y?Y?Y@Y@Y@Y?Y@Y@Y@Y?Y"@Y@Y"@Y?,Zgffff@@, ~ ,[? ,ZG,ffff@@,#,\\\\\\!~ ,"Z,#&,#,,## LL -PP -PX-Q -PX)-0!Fire suppression: advanced agents*-0"New Agent That Replaces Halon 1301f-R"@R?R?R?R@R@R@R?R@R@R@R?R@R@R"@R?-SL@@- ~ -T? -SG-TL@@-#-UUUUUU!~ -"S-#,-#--## LL.ggg .XX .XX*.9"Platform-aligned structural breaksO.9GLarge Aircraft Component Breaks Match Leading and Trailing Edge Angles.f.Y"@Y?Y?Y?Y@Y@Y@Y?Y@Y@Y@Y@Y"@Y@Y@Y?.Zgfffff<@...3L @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @L~ .[? .ZG.fffff<@.#..3 LL.\\\\\\!~ ."Z.# .#..## LL/ddd /PX /PX/0Airframe deice systems-/0%New Methods for the Eleviation of Icef/R"@R?R"@R?R@R@R@R?R@R@R@R?R"@R@R"@R?/SfffffD@/.~ /T? /SG/TfffffD@/#. /UU /U /UUU!~ /"S/#./#//## LL0999 0hX 0hX-09%UCAV/UAV (Sensors LO Characteristics)g09_Passive and Non-Detectable Sensors, Including Embedded Sensors and Frequency Selective Surfacesf0Y"@Y?Y@Y@Y@Y@Y@Y@Y@Y@Y?Y"@Y"@Y@Y"@Y?0ZLD@0.~ 0[@ 0ZG0^@#.0\\\\\\!0"Z#1000 1iX 1iX'10UCAV/UAV (Sensors Integration) &10Shared Resources and Aperturesf1R"@R"@R"@R@R@R@R@R"@R@R@R"@R"@R"@R@R"@R"@1ŠQ@1.~ 1T@ 1SG1T23333Sj@0.1UUUUUU!1"S#2999 2hX 2hX-29%UCAV/UAV (Weapons LO Characteristics)"29Shaped and Treated Weaponsf2Y"@Y?Y?Y@Y@Y@Y@Y"@Y"@Y@Y@Y?Y"@Y@Y"@Y@2ZfffffF@2.~ 2[? 2ZG2ffffF@1.2\\\\\\!2"Z#3111 3jX 3jX&31UCAV/UAV (Weapons Integration)331+Use of Intellegent, Reduced Size Munitions f3k"@k?k?k@k@k@k@k@k"@k@k@k@k@k@k"@k@3lC@3.~ 3m@ 3lG3mgfffff]@3#.3nnnnnn!~ 3"l3#/ D3"D3N43333323qrrqqqqqqqqqqrrrststuuuuuvs#N53333323qrrqqqqqqqqqqrrrststuuuuuvs#6WL/FIB6wWL/FIM6wWL/FIG6wWL/FIV6wWL/XPN6wLockheed%64LM FATE Proposal Technologies6B Description6xyyxxxx6 Attributes.6xxxxxyyyz{z{|||||}z#7 Structures7E Aeromechanics7E Flt Controls7E Subsystems7E7EMartinB75C# 8X 8X 8  8X8 8X86Advanced Compact InletY88QCompact, Fixed Geometry Inlet System for Reductions in Aircraft Volume and Weightf8"@"@"@"@@@@"@@@@@"@@"@"@8SffffffQ@888O L @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @L~ 8T"@ 8SF8T33333@8#88P LL 8UX 8UX 8UX 8UX8 U 8!UX~ 8"S@8#x@M8#88## LL 9X 9X9 9X 9X 9X 9<Conformal Fluidic Nozzle9>f9"@"@"@?"@"@"@"@@@@"@"@@"@"@9Zfffff&S@999ML @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @L~ 9[@ 9ZG9@9#99M LL 9\X 9\X 9\X 9\X9 \ 9!\X~ 9"Z@9#@3 D9D9" :X :X: :X :X :X:=Diverterless Inlet:N~Eliminates Inlet Actuation. Eliminates Diverter/Bleed/Bypass. Improves Maintainance, Weight, RF Signature and O&S Requirementsf:"@"@"@"@@@@"@@@@"@"@@"@"@:SQ@:9~ :T@ :SF:Tgffffj@:#9 :UX :UX :UX :UX : UX:!U~ :"S@:#@9 D:"D:; ;X ;X; ;X ;X;<TaillessO;GNo Vertical or Horizontal Tails for Low Drag and Excellent LO Qualitiesf;"@@@@@?@@@@@@"@@"@"@;ZLH@;8~ ;[@ ;ZF;u@;#8 ;\X;\ ;\X ;\X ; \\!~ ;"Z@;#@H;#;;## LL <X <X <X< <X <X <=Innovative Aero ControlsD<N<Aerodynamic Control Effectors for Vertical Tailless Aircraftf<"@@@@"@"@"@@@@@@"@@"@@<SI@<8~ <T"@ <SF<Tfffff}@<#8<UUUU < UX <!UX~ <"S@<#fffff@;<#<<## LL =X =X =X= =X =X&=@Continuous Moldline Technology=LxStructurally Sound Memory Elastic Material with Application to Expandable Fuel Tanks and Weapons Bays, Control Surfaces.f="@@@@"@"@"@@@@@@"@@"@@=ZI@=8~ =["@ =ZF=ffff}@=#8=\\\\ = \X =!\X~ ="Z@=#fffff@K=#==## LL >X> >X >X> >X>6Integrated VMSz>7rCommon Processors, Optical Buses to Integrate Flight and Propulsion Control, Actuators, Subsystems, Air Data, IFPCf>"@"@"@"@@@"@@@"@@"@@"@"@"@>S433333S@>8~ >T@ >SF>Tl@>#8 >UX >UX >UX >UX > UU!~ >"S@>#̌@@>#>>## LL ? ?X ? ?X$?<Integrated Adaptive Controls?Technologies include On-Line Control Allocation and Optimization, Parameter Identification and Control Design, Pilot Command Limitingf?"@@@@"@"@@@@"@@"@"@@"@@?ZLK@?8~ ?[@ ?ZF?@?#8 ?\X?\ ?\X ?\\\!~ ?"Z@?#33333@<?#??## LLDt<l,prRR|2,)@$bVA$fB$\ZVC$fD$\VE$ZfF$\VG$\fH$\VI$fJ$bVK$fL$VM$\fN$VO$f@P$o`Q$PVS$Pf]$o @ @X @ @X0@=(Rapid Prototyping Flight Control Systems[@?STailored to Improve Flight Control System Modularity and to Reduce Development Costf@"@"@"@@@@@@@"@"@@@@"@@@SN@@8~ @T@ @SF@T s@@#8 @UX@U @UX @UUU!~ @"S@@# @?@#@@## LL AX A A A AX!A@Robust Composite/SandwichNAAFReduced Weight, Elimination of Fasteners and Lower Manufacturing CostsfA"@"@"@@@@@"@@@@@@@"@"@AZP@AAAPL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @L~ A[@ AZFA@A#8 A\X A\XA\ A\X A \\!~ A"Z@A#@NA#AA## LL BX B B B BXB6Innovative Prototyping/B7'Minimal Tooling and Reduced Part CountsfB"@"@"@?@@@"@@@@@@@"@?BSL@BBBLL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @LL @L~ BT@ BSFBTq@B#8 BUX BUXBUUUU!~ B"S@B#@LB#BB## LL CX C C  CX CX$C@Composite Afford InitiativesgC_Use Large Unitized Structural Composite Parts to Minimize Hand Labor, Part and Fastener Count. fC"@"@"@"@@@"@@@@@@@@@"@CZN@CA~ C[@ CZFC@C#8 C\X C\XC\ C\X C \\!~ C"Z@C#gffff6@PC#CC## LL DX D DXD DXD=Integrated Subsystems7DN/Combining of Subsystems to Eliminate ComponentsfD"@"@"@"@@@@"@@@@"@"@"@"@"@DSLR@DB~ DT@ DSFDT43333sk@D#8DU DUXDU DUX D UU!~ D"S@D#43333s{@GD#DJ## LL EX E EXE EX'E<Integ Subsystem Routing ChanneljE>bA Structural Channel Running Longitudinally in the Vehicle Where All Wiring and Systems Can Be RunfE"@"@"@"@@@@"@@@@"@"@@@"@EZYP@EB~ E[@ EZFEffffh@E#8E\ E\XE\ E\X E \\!~ E"Z@E#gffffx@D DE"DE FX F  FXF FX FXF=Active Aeroelestic WingKFMCUse Aeroelastic Flexibility with Leading and Trailing Edge Devices.fF"@?@"@@@"@?@?@?@@"@@FSLE@F8~ FT@ FSFFT43333_@F#8 FUUU FUX F UX F!UX~ F"S@F#gffffw@8F#FF## LL G G GXG GXG<More Electric Aircraft=G5Replacing Many or All Hydraulic Systems with ElectricfG"@?"@"@@@@@@@@"@"@"@"@"@GZM@GB~ G[@ GZFG@G#8G\ G\XG\ G\X G \\!~ G"Z@G#433333v@JG#GG## LLH HX HX H HXH=Pneumatic ControlHH?@Use of Pneumatics for Vehicle Control and Boundary Layer ControlfH"@@??@"@@??@@?"@@"@?HSB@H8~ HT@ HSFHTgffff[@H#8 HUUU HUX H UX H!UX~ H"S@H#t@OH#HH## LLI IX IX I IXI@ MEMS ControlxIpMicromechanical Devices for Viscous Drag Reduction, Control Effectors, Active BL Control and Vortex ManipulationfI?@?"@@"@"@@@@?@"@@"@"@IZfffffG@I8~ I[@ IZAI@I#8I\\\\ I \X I!\X~ I"Z@I#q@>I#II## LL JX J J J JX(J= Laser Formed Metallic StructuresoJNgGeneration of Structures Using Laser Beam Solidification of Metallic Powders Without the Use of ToolingfJ"@"@"@?@@@"@@@@@@@"@?JSL@JB~ JT@ JSGJTq@J#8 JUXJUUUUU!~ J"S?J#q@BD#K KX KXK KX KX&K<Riblets/Paintless TechnologieseK>]Sheet Material and Other Techniques Applied To Aircraft Surface To Reduce Turbulent IntensityfK"@?"@"@@@@@@@@"@"@@"@@KZ33333I@K8~ K[? KZFK@K#8K\ K\X K\\ K \X K!\X~ K"Z@K#fffffFc@IK#KK## LL LX L L  LX LXL=Inflatable Structures{L?sA Continuous Moldline Technology with Variable Camber, Variable Inlet Lips and Conformal Fuel Bladder ApplicationsfL"@??@@@@???@?@@@?LS9@LB~ LT@ LSGLTR@L#8LUUUU L UX L!UX~ L"S@L#b@CL#LL## LLM MX M MX MXM<Natural Laminar Flow@MO8Passive Control For The Reduction of Turbulent IntensityfM"@@"@"@@@@@@@@?@@"@@MZfffffH@M9~ M[? MZFMffffH@M#9 M\\\ M\X M \XM!\~ M"Z@M#fffffX@:M#MM## LL N NXN NX NX&N6Affordable LO Air Data SensorshNK`Measures Critical Air Mass Flow Properties Based on Aerosol Particle Structure of the AtmospherefN"@"@@@@@@@@@@@"@"@"@@NSI@NA~ NT? NSFNTI@N#8NUUUUU  N!UX~ N"S?N#I@=N#NN## LLO OX O OXO< Coupled WingsXO>PInduced Drag is Reduced by Coupling Wing Tips, Thereby Increasing Effective SpanfO??"@"@?@@?@?@??@@?OZ:@O8~ O[? OZFO[:@O#8O\\\\ O \XO!\~ O"Z?O#:@FO#OO## LL P P P  PX PX&PPlanform Aligned Struct BreaksOPGLarge Aircraft Component Breaks Match Leading and Trailing Edge Angles.fP"@???@@@?@@@@"@@"@?P433333A@PA~ P? PGP433333A@P#8 P P!~ P"P#AP#PP## LLSG ] ,U$|t! > "  Oh+'0( hp FATE 1 Technology Matrix FATE ProgramXB Derek ByeLMTASMicrosoft Excel@hѿ@lG'+_G    f """)))UUUMMMBBB999|PP3f333f3333f3ffffff3f̙3ff333f333333333f33333333f33f3ff3f3f3f3333f33̙33333f333333f3333f3ffffff3f33ff3f3f3f3fff3ffffffffff3ffff̙fff3fffff3fff333f3f3ff3ff33f̙̙3̙ff̙̙̙3f̙3f333f3333f3ffffff3f̙3f3f3f333f3333f3ffffff3f̙3f3ffffffffff!___www45'  ' f-  "-"f" "- !f"-<<#- !#<-RR#- !#R-hh#- !#h-#- !#-#- !#-#- !#-#- !#-#- !#-#- !#-66#- !#6-77#- !#7-XX#- !#X-zz#- !#z-#- !#-#- !#-#- !#-- !-- !-- !-PP- !P-  - ! -- !-~~- !~-'- f#-   "-<#<- !\<#-R#R- !\R#-h#h- !\h#-#- !\#-#- !\#-#- !\#-#- !\#-#- !\#-#- !\#-6#6- !\6#-X#X- !\X#-z#z- !\z#-#- !\#-#- !\#-#- !\#-t#t- !\t#-u- !^-u- !^-PuP- !^P- u - !^ -u- !^-~u~- !^~-  !t#-  !Y} !|! !v} "-v- !v-v- !v-vPP- !vP-v  - !v -v- !v !$ !N53ff- 3ff !s$-'- 3fffArial-   2 &" -  "-"- ! -!!- !!-"- !-  - ! --  2 & "<1 2 ? >"R2 2 U T"h3 2 q j"4 2 "5 2 "6 2 "7 2 "8 2  "9 2  "610 2 C 9"X12 2 e Z"z13 2  |"14 2  "15 2  "16 2 ` "t17 2 z$A 2 4B 2 PC 2 R D 2 b E 2 ~F  "Systemn-'- f#Arial-  ArialT-  2 'Revision   2 810/28/97   Arial- -'-  6#  2 'Key-'-  f#ArialU- Arial- - -   !!7 !!7 !!7 !!7 !!7O !!7Q--'- - X7#- - - -    2 8'9 - I2 9C,Positive/Improvement/>150lb Weight Reduction - --'- - f#- -    !!Y !!Y--'- - zY#- - - -    2 Z'3 - !2 [CNeutral/No Change - --'- - f#- -    !!{ !!{ !!{ !!{ !!{O !!{Q--'- - {#- - - -    2 |'1- F2 };* Negative/Decrement/>150lb Weight Increase  - --'- - f#Arial-Arial--   ! ! ! ! !O !Q--'-- #----  *2 'FWV Demonstrator Totals      -@2 D& = Sum(Attributes X Weighting Factors)          ---'-- f#- -   ! ! ! ! !O !Q !  !  ! !--'-- #- -- -  32 'FWV Tech Demo (Goal Weighted)     - ^2 : = Sum(Attributes X Weighting Factors) X COF X Goal Totals              ---'-- f#- ---'-- f#- -- -- - 2 &' Baseline for    2 C' Comparison  - 2 C: 2 `' Unmanned   "2 }'Vehicle with F-22      2 ' or F/A-18E/F  2 '1995 2 'Technologies,    2 ' UAV Ground  2 'Control Station     ---'-- f#--'- f-  "-- !-f- !f--4'՜.+,08@ X` h {Lockheed Martin Sheet1  Worksheets  !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRTUVWXYZ[\]^_`abcdefgijklmnoRoot EntryynthesisADVSYN~1B@B6F (*.prn)m?(ComBooked) (*.csv)05x@<@201059\dByx@<@.C 8CSummaryInformationxB(S(DocumentSummaryInformation8h