Statement
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Developmenthistory
Developmentbackground
Inthe1970s,whentheColdWarwasinfullswing,theSovietUnionvigorouslydevelopedvariousmedium-andlong-rangeairdefensemissilesandhigh-altitudehigh-speedhomelandAirdefenseinterceptors,suchasS-200(NATOcodename:Sam-5)medium-highaltitudeultra-long-rangesurface-to-airmissiles,S-300(NATOcodename:Sam-10)all-airspaceairdefensemissilesystemsandMiG-25/31High-altitudesupersonicinterceptionfighters,etc.InordertocovertlybreakthroughtheSovietairdefensenetwork,findanddestroytheSovietUnion’sintercontinentalballisticnuclearmissilelaunchbaseandotherimportantstrategictargets,theUSAirForceproposedtobuildanewstrategicbomber,emphasizingdefensepenetrationcapabilitiesandrequiringtheabilitytoavoidairdefenses.Radardetection,diveintothedepthoftheenemy,andcompletethemissionwithan80%successrate.Tothisend,theAirForcedraftedthe"SaberPenetrator"plan,andincludedtheapplicationofstealthtechnologyonthespecificagenda.
Constructionhistory
Planconfirmed
InAugust1975,theUSDepartmentofDefenseAdvancedResearchProjectsAgency(DARPA)invitedLockheed,BoeingandNorthropprovidepreliminaryengineeringdataforalow-detectabilityaircraft.BecausetheprototypesubmittedbyLockheednotlongagowaswellreceived,theAirForcehandedoverthecontractfortheproductionoftheF-117stealthfightertothiscompany.Withtheproductionofstealthfighters,theU.S.DepartmentofDefenseandcongressionaldignitariesbegantoaccepttheconceptof"stealthbombers",andin1977formallyapprovedtheAirForce’sapplicationforthedevelopmentofthisaircraft.In1978,theCarteradministrationsecretlyauthorizedthelaunch.ThestealthbomberprojectisnamedAdvancedTechnologyBomber(ATB).ThisistheoriginalnameoftheB-2stealthstrategicbomber.ItaimstodevelopabomberthatcanreplacetheB-1A.
Theplanisannounced
InSeptember1980,theUSAirForceissuedtheATBRequestforProposal(RFP),duetothecostandtechnicalaspectsoftheproject.Severechallenges,sotheAirForceencouragescooperationbetweenaerospacecompanies.Sotherearetwomajorcompetingcamps-LockheedandRockwellteams,Northrop,BoeingandLing-Temko-Water(LTV)teams.ThesituationchangedafterPresidentReaganwaselectedonJanuary20,1981.TheReaganadministrationincreaseditsdefenseinvestment,enoughtosupportseveralmilitaryresearchprojects,includingnewstrategicbombers.OnOctober2,1981,PresidentReaganannouncedthestartoftheStrategicModernizationProject(SMP),purchasing100B-1Bs.TheATBwasalsosecretlydevelopedaspartoftheSMP.Atthattime,thetotaldemandwasexpectedtoreach132aircraft.OnlyafewinsidersknewthattheU.S.AirForcewasdevelopingtwostrategicbombersatthesametime.
Designconfirmed
Northrop'sprogramcodeis"SeniorIce"(SeniorIce,thesecretwordhasnospecificmeaning),Lockheed'sprogramcode"SeniorPeg"(SeniorPeg)."PremiumDiamonds"ishostedbyWilcoE.Gasic,SeniorVicePresidentofNorthropAdvancedPlanning,andtheplanningdirectorisHalMarkalyan.Lockheed/Rockwell’s"advancednail"programhasnotdisclosedmuchinformation,butinviewofLockheed’sachievementsinstealthtechnologyatthattimeandRockwell’sexperienceintheB-1project,itisgenerallybelievedthatTheteamwillwinthecompetition.However,onOctober20,1981,theU.S.AirForceannouncedthatNorthropwasthewinneroftheATBcontract,theaircraftnumberedB-2,andsignedaninitialcontractfor6testflightaircraftandtwostatictestaircraft,plus127productionbombers.Theintentiontoorder,planstoachieveinitialoperationalcapability(IOC)in1987.
Inthedivisionoflaborbetweenthethreecompanies,Northropisresponsibleformanufacturingthefrontcenterfuselageandcockpit,thefrontandrearedgesoftheaircraft,andthecontrolwingsurface.Itisalsoresponsibleforthefinalassemblyandoverallcoordinationoftheplan.Boeingisresponsibleformanufacturingtherearcenterfuselageandbombbay,aswellastheouterwingsectionandlandinggear.LTVisresponsibleformanufacturingthemid-wingsectionandtailnozzlesincludingtheenginecompartment(LTVwaslateracquiredbyNorthropGrumman).ThefinalassemblywascarriedoutatYard4oftheU.S.AirForcePlant42inPalmdale,California.
Buildquantity
AV-1 | 82-1066 | AmericanPhantom | Inservice |
AV-2 | 82-1067 | ArizonaGhost | Inservice |
AV-3 | 82-1068 | NewYorkPhantom | Inservice |
AV-4 | 82-1069 | IndianaGhost | Inservice |
AV-5 | 82-1070 | OhioGhost | Inservice |
AV-6 | 82-1071 | MississippiPhantom | Inservice |
AV-7 | 88-0328 | TexasPhantom | Inservice |
AV-8 | 88-0329 | MissouriGhost | Inservice |
AV-9 | 88-0330 | CaliforniaGhost | Inservice |
AV-10 | 88-0331 | SouthCardSpectre | Inservice |
AV-11 | 88-0332 | WashingtonPhantom | InFebruary2010,therewasafireintheenginecompartmentandthebodywasseverelydamaged.Itisbeingrepaired. |
AV-12 | 89-0127 | KansasGhost | WreckandcrashonFebruary23,2008 |
AV-13 | 89-0128 | NebraskaPhantom | Inservice p> |
AV-14 | 89-0129 | GeorgiaGhost | Inservice |
AV-15 | 90-0040 | AlaskaGhost | Inservice |
AV-16 | 90-0041 | HawaiianGhost | Inservice |
AV-17 | 92-0700 | FloridaGhost | Inservice |
AV-18 | 93-1085 | OklahomaPhantom | Inservice |
AV-19 | 93-1086 | KittyEagleGhost | Inservice |
AV-20 | 93-1087 | PhantomGhost | Inservice |
AV-21 | 93-1088 | LouisAnnaPhantom | Inservice |
AV-22toAV-165 | Cancel |
Technicalfeatures
Modelstructure
ThefinalNorthropdesignisapureflyingwing,noverticaltailorrudder,Fromabove,theB-2lookslikealargeboomerang.TheoutlineoftheplanviewofB-2consistsof12straightlinesparalleltoeachother.Theleadingedgeofthewingisparalleltothetrailingedgeofthewingandthewingtipontheotherside.Themiddlepartoftheaircraftisraisedtoaccommodatethecockpit,bombbayandelectronicequipment.Theprotuberancesonbothsidesofthecentralfuselageareenginecompartments.Theserratedairinletsarearrangedonthebackoftheflyingwing.Twoturbofanengineswithoutafterburnerareinstalledineachenginecompartment.Thewingtipsarenotparalleltothedirectionoftheairflow,butarecuttobeparalleltotheleadingedgeoftheotherwing.Exceptforthewingtips,theentireouterwingsectionhasnotaperandisaconstant-chordwing.TherearedgeofthefuselagetailisW-shapedserrated,andtheedgesarealsoparalleltothefrontedgesofthewingsonbothsides.Sincetheleadingedgeofthewingoftheflyingwingisinfrontofthefuselage,inordertomaketheaerodynamiccenterclosetothecenterofgravity,thewingalsoneedstobesweptback.
TheB-2centralfuselageneedstobedeepenoughtoaccommodatethecockpitandbombbay,butthelengthshouldbeasshortaspossibletoavoidexcessiveresistanceathighsubsonicspeeds.Thechordlengthoftheouterwingofthecentralfuselageisdeterminedbytheenginecompartmentandthestealthairinletandtailnozzle.WhentheB-2fliesathighsubsonicspeeds,thethicksupercriticalairfoilacceleratestheairflowontheuppersurfaceofthewingtosupersonicspeed.Exceptfortheareabehindthetailnozzle,9largecontrolwingsurfacesarearrangedontherearedgeoftheentireflyingwingoftheB-2.Thelast"beavertail"isawholemovablecontrolsurfaceusedtooffsettheturbulencecausedbyverticalgustswhenflyingatlowaltitudes.Ontheoutermostsideisapairofsplitairfoilcalled"speedbrake-rudder".Theremaining6aileronsurfacesareruddersurfacesforpitchandrollcontrol,andtheoutermostpairalsodoublesasaileronsatlowspeeds.
Aerodynamicdesign
TheB-2doesnothaveaverticaltail,whichisdifferentfromtraditionalaircraft.Theaircraftisyawneutral,whichmeansthatwhentheB-2turnstotheleftorright,itwillnotgenerateaerodynamicforcetoreturntothecenter.B-2iscontrolledbyNorthrop'spatentedairbrake-rudderonthetrailingedgeoftheouterwing.Theairbrake-ruddercanbecrackedontheupperandlowersides.Atthesametime,thecrackisusedasaspeedbrake,andwhenitiscrackedasymmetrically,itcanbeusedasarudder.Duetotheexistenceoftheboundarylayeronthesurfaceoftheflyingwing,thespeedbrake-ruddermustbecrackedatleast5degreestobeeffective.Therefore,innormalflight,theairbrakesandruddersonbothsidesareintheopenpositionof5degrees,andtheycanworkimmediatelywhentheyneedtobecontrolled.ThisiswhyweseetheairbrakesandruddersintheB-2flightphotos.It'sallthereasonsforopening.However,theopenairbrake-rudderwillaffectthestealtheffectoftheaircraft,sowhentheB-2arrivesinthebattlezone,theairbrake-rudderwillbecompletelyclosed.
MostofthesurfaceofB-2Aiscoveredbyalayerofspecialelasticmaterialtomaintainuniformelectricalconductivityonthesurfacetoreducethereflectionofradarwavesfromjointsorjoints.Inthedesign,thepartsthatcannotrelyontheshapeforstealth(suchastheairinlet)mustbecoatedwithradarabsorbingmaterial(RAM),anditscompositionisstillhighlyclassified.RAMisacoatingthatcanbesprayedinmultiplelayersandcontainscomponentsthatconvertradarwaveenergyintoheatenergy.Aftertheentiremachineiscoatedwithacoatingofappropriatethickness,aftertheradarwavesofaspecificwavelengthareirradiatedtothecoating,theradarwavesreflectedonbothsidesofthecoatingwillinterfereandcanceleachotherout.Asimilarconceptisthecoatingofopticallenses,whichcaneliminateunnecessarylight.
Powerdesign
FourGEF118-110non-afterburningturbofanenginesareinstalledintheenginecompartmentsonbothsidesofthecentralfuselageofB-2A,eachwitharatedstaticthrustof8,618kg.F118isdevelopedonthebasisofF101-X,whichisafightermodeloftheF101engineoftheB-1bomber.ComparedwithF101,F101-Xhasasmallerlow-pressureexternalculvertcasing,whichreducesthebypassratiofrom2:1to0.87:1.Theenginewithlowbypassratioonlyneedssmallerintakeandexhaustsystems,soitwasselectedbyB-2.Theengineairintakeisfarawayfromtheleadingedgeofthewingtoavoidbeingirradiatedbyradarwavesfrombelow.Duetothethickflyingwingstructure,theB-2canburytheenginedeeplyintheflyingwing.Theflatairinletandcurvedairinletontheuppersurfaceoftheflyingwingcanensurethattheairborneradarcannotdirectlyilluminatefromabove.Thefrontoftheengineisevenmoreimpossiblefrombelow.Inthisway,theB-2canuseasimplerairinlet,andonlyneedtomakeasharptoothmodificationonthelipandthereisnoproblem.
B-2airinletboundarylayerseparationplateseparatestheboundarylayerairflowandthenismixedintothetailnozzletoreducetheexhausttemperatureandreduceinfraredradiation.Theairflowpassingthroughtheseparationplateisalsodiffusedanddirectedtovariousinternalairflowpipelineswhicharecollectivelycalledthesecondaryairflowsystem.Thisincludestheaccessorydriveinstalledonthebodyandtheventilationoftheenginecompartment,theramcoolingairflowoftheheatexchangeroftheenvironmentalcontrolsystemandtheairflowofthebypasscircuit.Whenworkingatlowspeedsandontheground,thefourdiamond-shapedengineauxiliaryintakevalveslocatedonthetopoftheintakeductcoveranddirectlyinfrontofeachengineinletincreasetheairflowtotheengine.Theoperationwiththeauxiliaryintakevalveopenedreducesthemassflowratioofthemainintakeportandthecorrespondingturninglossofthesharplip.
AvionicsDesign
TwocrewmembersoftheB-2AsitsidebysideontheACEIIejectionseat,withthepilotontheleftandthemissioncommanderontheright.Thereare4largewindshieldsonthefrontandonbothsidesofthecockpit.Theoccupantsenterandexitthecockpitthroughthebellydoor.Inanemergency,theejectionseatisejectedthroughthefragiledooronthetopofthecockpit.Themissioncommanderisresponsiblefornavigationandweapondelivery,butbothcrewmemberscancompletetheentiremissionindividually.Thereare4colorCRTmonitorsinfrontofeachoccupant,adatainputpanelontherightandasetofthrottlesontheleft.Thereisalsoathirdcrewseatbehindthecockpit,butitisrarelyused.Theseatalsohasanejectionseatwithafragilehatchonthetop.TheB-2A'snavigationsysteminitiallyconsistsoftwosets,eachofwhichcanbenavigatedindividually,buttheaccuracywillbehigherwhenworkingtogether.Oneisaninertialmeasurementunit,andtheotherisaNorthropNAS-26astronomicalinertialunit.NAS-26wasoriginallydevelopedforghostlong-rangecruisemissiles.Itisaphotoelectrictelescopesystemwithastablebasethatcanlockpre-selectedstarsonacloudyday.Theobservationwindowofthesystemisontheleftsideofthewindshield.
TheB-2AairborneradarisAN/APQ-181phasedarrayradar,manufacturedbyHughes.Thiskindofphasedarrayhas2radarantennaarrays,whichischaracterizedbynoneedtoaddarotatingorswingingantenna,andonlythroughthechangeandcombinationofthesignalarrayposition,itcanscandifferentanglesanddifferentdirections.Itsworkingfrequencyis12-18GHZ,thesidelobeissmall,andtheabilitytoresistelectronicinterferenceisstrong.Thereare21workingmodes,themostprominentonesaresyntheticapertureradarworkingmodeandanti-syntheticapertureradarmode.Theformerismainlyusedtoscanlandformsandcanclearlyobtainscannedimagesofthesurfacewithinadistanceof161kilometersforaircrafttousewhenbombinggroundtargets;thelatterismainlyusedtoidentifyandcaptureseatargets,withthelongesteffectiverangeavailable.Upto128kilometers.Inaddition,theB-2Abombercanuseterrainmatchingandterrainavoidancetechnology,sothatitcanpenetrateintotheenemy'sairspaceatlowaltitudetoperformbombingmissions.
Armedloading
ThetworotatingmagazinesoftheB-2bombercancarry16AGM-129cruisemissiles,andcanalsocarry80MK82or16MK84Ordinarybombsor36CBU-87clusterbombscancarry16bombswhenusingthenewTSSMlong-rangeattackammunition.Whenusingnuclearweapons,itcancarry16B63nuclearbombs.Inaddition,theAGM-129cruisemissilecanalsobeloadedwithnuclearwarheads.InFebruary2002,B-2increasedtheabilitytouseJASSMair-to-surfacemissilesoutsidethejointdefensezone.Mostofthespaceinsidetheouterwingsectionisoccupiedbythefueltank.Twolargebombbaysarearrangedsidebysideunderthefuselagebetweentheenginecompartments.Eachbombbaycanbehungwithanadvancedrotatingpylondevelopedbycarriersound,whichcanmount8pieces.For908kgammunition,twobombrackcomponentscanalsobeinstalledtomountconventionalammunition.Aftertheavionicsandequipmentperformanceisimproved,theB-2AcancarrytheAGM-154combinedrangeweaponandtheGBU-285,000-poundlaser-guidedbomb;inaddition,itcanalsocarrytheAGM-158combinedair-to-surfacerangemissile.
40,000lbs(18,000kg):Mk82500lbslow-resistancegeneralpurposebombscarriedbystackablebombracks(totalnumberofcarryis80)
27,000pounds(12,000kg):750-poundclassclusterbombscarriedbystackablebombracks(36piecesintotal)
16RotaryLauncherAssembly(RLA):Itcancarry2,000-poundweapons(suchasMk842,000-poundlow-resistancegeneralpurposebomb,GBU-31jointdirectattackammunition,orB-61andB-83nuclearbombs).
Performancedata
Referencedata | |
Length | 21.0m |
Wingspan | 52.4m |
Height | 5.18m |
Wingarea | 478squaremeters |
Emptyweight | 71700kg |
Normaltake-offweight | 152200kg |
Maximumtake-offweight | 170600kg |
Engine | 4×GeneralElectricCompanyF118-GE-100turbofanengine |
Thrust | 4×17,300pounds |
Maximumfuelquantity | 75750kg |
Referenceperformance |
---|
0.95Mach |
23,000kg |
15,200m |
6,000nauticalmiles(11,100kilometers) |
329kg/m² |
0.205 |
Servicedynamics
ThefirsttimetheB-2bomberwasputintoactualcombatItwastheKosovoWarinSerbia,andthiswasthefirstbattleaftertenyearsofservice.OnthenightofMay7,1999,localtime,andonMay8,1999,Beijingtime,theB-2bomber,whichwasputintoactualcombatforthefirsttime,usedthreeprecision-guidedbombstodirectlyhittheEmbassyofthePeople’sRepublicofChinainBelgradeandwaskilledonthespotfromXinhua.ThreeChinesejournalists,ShaoYunhuanoftheagency,XuXinghuandZhuYingofGuangmingDaily,woundeddozensofpeopleandcausedseriousdamagetotheembassybuilding.OneoftheJDAMsdidnotexplodeonthespot,andwasnotremovedanddestroyedbytheSerbiansideuntilfiveyearslater.Afterthat,theChinesesidebelievedthatthiswasadeliberatebombing,possiblyinretaliationforChina’spreviousoppositiontoNATO’sbombingoftheYugoslavia,andthereforelodgedastrongprotesttotheUnitedStates.NATOexplainedthatitwasanaccidentalbombing.
Thebombingandsubsequentdevelopmentscausedasuddendeteriorationintherelationsbetweenthetwocountries,whichwereoriginallyintheascendingphaseduetotheexchangeofvisitsbetweentheheadsofstateofChinaandtheUnitedStates.Aftertheincident,theChinesepeoplewereveryangry.ManycollegestudentsdemonstratedinfrontoftheembassiesoftheUnitedStatesandotherNATOcountriesinBeijing,Shanghai,Shenyangandotherplaces.Theparadeshowedsignsoflossofcontrolinthelaterperiod,includingtheburningofAmericanfastfoodrestaurantsandthedestructionofAmericanembassiesandconsulates.Wait.Duringtheincident,theUSConsulateinHongKongalsoencountereddemonstrationsbyHongKongpeople.RelationsbetweenChinaandtheUnitedStatesbegantograduallyrecoverattheendof1999,andNATOprovidedfinancialcompensationtothevictims.ThethenPresidentoftheUnitedStatesBillClintonpersonallyapologizedfortheincidentandcompensatedforthedamagedpremisesinChina.TheChinesegovernmentalsocompensatedtheAmericanpremisesdamagedbytheprotesters.
InMarch2003,theB-2wasputintotheIraqibattlefield.AB-2droppedtwo2130kgnew-typeEGBU-28guidedbombsforthefirsttimeontheeveningofthe28th,whichblewupthecityofBaghdad.AcommunicationstowerontheTigrisRiver.ThisisthelargestbombusedbytheUSmilitaryintheIraqWar.EGBU-28hasglobalpositioning/inertialnavigationandsemi-activelaserfull-rangedual-modeguidancemode,whichismoreadvancedthanpreviousJDAMbombs.EGBU-28caneffectivelydestroylargesolidtargetsandminimizecollateraldamage.DuringtheIraqWar,theB-2hadanon-refuelingrangeof11,119kilometers.TwoB-2sweretransferredtotheDiegoGarciaUSAirForceBaseintheIndianOcean.Fromthisbase,thebombingofIraqdidnotrequireaerialrefueling.
OnFebruary23,2008,anaircraftnumbered89-0127(namedtheKansasGhost)crashedduringtake-offatAndersonAirForceBaseinGuam.Thetwopilotsonboardwererescuedsafely.InvestigationsshowedthatbeforetheB-2bombertookoff,threeofthe24sensorsweredamagedbywatervapor,andthewrongatmosphericinformationwasmeasured,causingtheflightcontrolcomputertomiscalculatetherequiredflightspeedandascentanglefortakeoff.Althoughthetwopilotsontheplanetriedtocorrectthewronginformation,theywereunsuccessful,andtheplanerushedtothegroundandburstintoflames.
InFebruary2010,oneofthefourenginesoftheB-2bomber(No.88-0332)WashingtonPhantomfiredonthegroundatAndersonAirForceBaseinGuam,whichalsodamagedtheenginecompartmentandOtherparts.TheB-2wasrestoredtoserviceonJanuary9,2014.
OnMarch28,2013,theUSAirForcesenttwoB-2stealthbomberstoSouthKoreatoparticipateintheSouthKorea-USjointmilitaryexercise"Vulture."ThisisthefirsttimethattheUnitedStateshassentaB-2stealthbombercapableofcarryingnuclearweaponstotheKoreanPeninsulaforlive-fireexercises.ThetwoplanestookofffromWhitemanAirForceBaseinMissouriandflew13,000milesbackandforthina"singlecontinuousmission",droppingsimulatedammunitionwithinthetargetrangeofSouthKorea.TheexerciseangeredNorthKoreaandpromptedPyongyangtothreatentolauncha"full-scalewar"withtheaidofnuclearweapons.ConsideringthatNorthKoreahasbeenangeredbytheparticipationofB-52bombers,theuseofstealthbomberswillfurtheraggravatetensionswithPyongyang.
OnthemorningofOctober23,2018localtime,aB-2stealthbomberoftheUSAirForceencounteredanemergencyduringitsflightandmadeanemergencylandingatColoradoSpringsAirport.
Follow-upimprovements
InJune2003,theU.S.AirForceplannedtoaddLink-16totheB-2bomberinaccordancewiththeB-2super-horizoncommunicationplan.Datalink.TheapplicationofLink-16datalinkdatawillenabletheB-2pilottoknowthelocationoftheaircraftinrealtime.
OnSeptember10,2003,aU.S.AirForceplanedropped80227kgJDAMbombsatatestrangeinUtah,bombinglessthan1,609inlength.Metersofsimulatedsmallairport.EachJDAMbombhasbeenindividuallyprogrammedtoattackitsintendedtargetwithanidealangleandheading.
InAugust2004,NorthropGrummanofficialsstatedthattheywoulddeliverthefirstB-2bomberwithanewstealthcoatingtoWhitemanAirForceBase.ThismarksakeymilestoneintheB-2'sstealthandradarimprovementwork.
InDecember2004,atTinkerAirForceBase,Oklahoma,theE-3AirborneEarlyWarningandControlSystem(AWACS)fleetandthebase’sglobalTheForceBomberJointFlightTestTaskForcejointlyconductedtheLink-16datalinkcomprehensiveverificationtestontheB-2Astealthbomber.
InApril2006,engineersfromtheMaterialsandManufacturingCommitteeofWrightPattersonAirForceBaseinOhio,USA,togetherwiththeB-2systemteamandmaterialsexperts,Solvedakeymaterialmassproductionproblem.ThisproblemdirectlyaffectstheoperationalmaintainabilityoftheU.S.AirForce’sB-2bomberfleet,whichinturnaffectsoperationalavailability.
InSeptember2006,NorthropGrummanandRaytheonstatedthattheyhadproposedtotheU.S.DepartmentofDefenseanincrementalAgradualupgradepathtoimprovetheB-2inmanyyearstocome.
InOctober2006,NorthropGrummanhopedthatitsB-2AbombercouldbeusedasatestplatformfortheU.S.AirForce’s"nextgenerationlong-rangeattacksystem"."(NGLRS)requiredtechnologies,weaponsandoperationalconceptstobeverifiedandevaluated.
OnJanuary2,2007,theUSAirForcebomberdirectorstatedthattheAirForcehadcarriedoutaseriesofupgradestotheB-2stealthbomber.Someupgradeshavebeencompleted,somearestillbeingplanned,andsomewillbeplannedmorethan10yearsinadvance.
InMarch2007,theU.S.AirForcehasapprovedthemaincontractoroftheB-2stealthbomber,NorthropGrumman’sproposedimprovementtothisbomber.Theplanofthesatellitecommunicationsystemagreedwiththecompanytostartthedevelopmentandverificationofanextremelyhighfrequency(EHF)satellitecommunicationsysteminordertoincreasetheabilityoftheB-2stealthbombertosendandreceivebattlefieldinformationbyapproximately100times.
InJune2007,NorthropGrummanandBoeingsigneda62-month,US$171millionsystemdevelopmentandverification(SDD)contract.Thiscontractisthefirstincrementalupgradeprojectforthenewextremelyhighfrequency(EHF)satellitecommunicationssystemoftheU.S.AirForceB-2stealthbomber.
InJuly2007,NorthropGrummanannouncedthatthecompanyhadbegunresearchingthenew30,000-pound(13620kg)-classpenetratorweapon.
InNovember2007,NorthropGrummanhascompletedthedevelopmentofanewradarantennatestdevicefortheB-2StealthBomberRadarImprovementProgram(RMP)(DTU)installation,integrationandfirstflight.
InJanuary2008,theU.S.AirForce509BomberWingatWhitemanAirForceBaseinMissouriannouncedthatthebase’sweaponsexpertswillweighupto30,000pounds(13,620kg)ofgiantTheMassiveOrdnancePenetrator(MOP)iscarriedinthebombbayoftheB-2"Spirit"stealthbomber.
InJuly2008,NorthropGrummancompletedthedevelopmentofamoderncomputerarchitectureforupgradingtheflightmanagementsystem(FMS)oftheB-2AstealthbomberThefirststage.
InJanuary2010,theU.S.AirForceusedtheB-2Astealthbombertocompleteaflightverificationusingartificialmixedfuel.JeffBraun,directoroftheUSAirForce'sOptionalFuelVerificationOffice,revealedthatduringtheverificationprocess,aB-2tookofffromWhitemanAirForceBaseandcompletedatrainingsession.
InApril2010,NorthropGrummanhascompletedthesystemdevelopmentanddemonstrationphase(SDD)oftheB-2bomberradarmodernizationproject(RMP).
InMarch2012,thePentagonannounceda10-yearplantomodernizeandimprovetheB-2forceworth20billionU.S.dollars.Themainareaofimprovementisthecompletereplacementofoutdatedavionicsandequipmentprocedurestodealwiththeincreasinglycomplex"potentialenemy"airdefensenetworkinthefuture.
WorldRecord
Themostexpensivemilitaryaircraft(unit):ThemostexpensivemilitaryaircraftintheworldismadeintheUnitedStatesTheB-2Valor,eachcostmorethan1.3billionU.S.dollars(780millionpounds).(GuinnessWorldRecords)