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Active Project (2013 - 2014) Solid-State Thermionic Nuclear Power For Megawatt Propulsion, Planetary Surface And Commercial Power Project Center Innovation Fund: JSC CIF (Also Includes JSC IRAD) Program Space Technology Mission Directorate ( STMD ) At Start: 2 Current: 2 At End: 4 1 2 3 4 5 6 7 8 9 Applied Research Development Demo & Test NASA/JSC Propulsion and Power Division Project Technology Maturity ABSTRACT Thermionic (TI) power conversion is a promising technology first investigated for power conversion in the 1960’s, and of renewed interest due to modern advances in nanotechnology, MEMS, materials and manufacturing. Benefits include high conversion efficiency (20%), static operation with no moving parts and potential for high reliability, greatly reduced plant complexity, and the potential for reduced development costs. Thermionic emission, credited to Edison in 1880, forms the basis of vacuum tubes and much of 20th century electronics. Heat can be converted into electricity when electrons emitted from a hot surface are collected across a small gap....Read more on the last page. Technology Area: Space Power & Energy Storage TA03 (Primary) In-Space Propulsion Technologies TA02 (Secondary) ANTICIPATED BENEFITS To NASA unfunded & planned missions: This project targets one the most critical barriers to human deep space exploration – the means to efficiently power and rapidly propel human missions to Mars and beyond. The project will explore the implementation of a high efficiency “Solid-State” Thermionic-based nuclear fission power systems to serve Electric Propulsion systems such as Q-thrusters, VASIMR, Hall, or other approaches. A Solid-State approach centered around advanced Thermionic power converters would combine the high efficiency of traditional dynamic power conversion (Rankine, Brayton, Stirling) with the simplicity of a static converter with no moving parts. The resulting system... Read more on the last page. Printed 4/4/2014 1 https://ntrs.nasa.gov/search.jsp?R=20140004416 2018-05-19T07:55:55+00:00Z

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ActiveProject(2013-2014)

Solid-StateThermionicNuclearPowerForMegawattPropulsion,PlanetarySurfaceAndCommercialPowerProjectCenterInnovationFund:JSCCIF(AlsoIncludesJSCIRAD)ProgramSpaceTechnologyMissionDirectorate(STMD)

AtStart:2 Current:2 AtEnd:4

1 2 3 4 5 6 7 8 9

AppliedResearch Development Demo&Test

NASA/JSCPropulsionandPowerDivision

ProjectTechnologyMaturity

ABSTRACT

Thermionic(TI)powerconversionisapromisingtechnologyfirstinvestigatedfor

powerconversioninthe1960’s,andofrenewedinterestduetomodernadvances

innanotechnology,MEMS,materialsandmanufacturing.Benefitsincludehigh

conversionefficiency(20%),staticoperationwithnomovingpartsandpotential

forhighreliability,greatlyreducedplantcomplexity,andthepotentialforreduced

developmentcosts.Thermionicemission,creditedtoEdisonin1880,formsthe

basisofvacuumtubesandmuchof20thcenturyelectronics.Heatcanbe

convertedintoelectricitywhenelectronsemittedfromahotsurfacearecollected

acrossasmallgap....Readmoreonthelastpage.

TechnologyArea: SpacePower&EnergyStorageTA03(Primary)In-SpacePropulsionTechnologiesTA02(Secondary)

ANTICIPATEDBENEFITS

ToNASAunfunded&plannedmissions:Thisprojecttargetsonethemostcriticalbarrierstohumandeepspaceexploration–the

meanstoefficientlypowerandrapidlypropelhumanmissionstoMarsandbeyond.The

projectwillexploretheimplementationofahighefficiency“Solid-State”Thermionic-based

nuclearfissionpowersystemstoserveElectricPropulsionsystemssuchasQ-thrusters,

VASIMR,Hall,orotherapproaches.ASolid-Stateapproachcenteredaroundadvanced

Thermionicpowerconverterswouldcombinethehighefficiencyoftraditionaldynamic

powerconversion(Rankine,Brayton,Stirling)withthesimplicityofastaticconverterwith

nomovingparts.Theresultingsystem...

Readmoreonthelastpage.

Printed4/4/2014 1

https://ntrs.nasa.gov/search.jsp?R=20140004416 2018-05-19T07:55:55+00:00Z

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DETAILEDDESCRIPTION

Thermionic(TI)powerconversionisapromisingtechnologyfirstinvestigatedforpowerconversion

inthe1960’s,andofrenewedinterestduetomodernadvancesinnanotechnology,MEMS,

materialsandmanufacturing.Benefitsincludehighconversionefficiency(20%),staticoperation

withnomovingpartsandpotentialforhighreliability,greatlyreducedplantcomplexity,andthe

potentialforlowDesign,Development.TestandEvaluation(DDT&E)costs.Thermionicemission,

creditedtoEdisonin1880,formsthebasisofvacuumtubesandmuchof20thcenturyelectronics.

Heatcanbeconvertedintoelectricitywhenelectronsemittedfromahotsurfacearecollected

acrossasmallgap.Forexample,two“small”(6kWe)ThermionicSpaceReactorswereflownby

theUSSRin1987-88foroceanradarreconnaissance.HigherpoweredNuclear-Thermionic

powersystemsdrivingElectricPropulsion(Q-thruster,VASIMR,etc.)mayofferthebreakthrough

necessaryforhumanMarsmissionsof<1yrroundtrip.

...

Solid-StateThermionicNuclearPowerForMegawattPropulsion,PlanetarySurfaceAndCommercialPowerProject

MANAGEMENT

ProgramExecutive:JohnFalker

ProgramManager:RonaldGClaytonProjectManager:JeffreyGeorge

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U.S.stateswithwork

Leadcenter:JohnsonSpaceCenter

Supportingcenters:GlennResearchCenter,MarshallSpaceFlightCenter,NASAHeadquarters

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Solid-StateThermionicNuclearPowerForMegawattPropulsion,PlanetarySurfaceAndCommercialPowerProject

DETAILEDDESCRIPTION(CONT'D)

Thisprojecttargetsonethemostcriticalbarrierstohumandeepspaceexploration–themeanstoefficientlypower

andrapidlypropelhumanmissionstoMarsandbeyond.Theprojectwillexploretheimplementationofahigh

efficiency“Solid-State”Thermionic-basednuclearfissionpowersystemstoserveElectricPropulsionsystemssuch

asQ-thrusters,VASIMR,Hall,orotherapproaches.ASolid-StateapproachcenteredaroundadvancedThermionic

powerconverterswouldcombinethehighefficiencyoftraditionaldynamicpowerconversion(Rankine,Brayton,

Stirling)withthesimplicityofastaticconverterwithnomovingparts.TheresultingsystemcouldenableHuman

Marsmissionsof<1yearroundtripbyaffordingasystemofmegawattpower,lowspecificmass(<10kg/kWe),

greatlyreducedplantcomplexity,andassociatedsavingsindevelopmentcost.

Thisprojectprovidestheinitialfoundationandconfidenceforhighefficiencysolid-statepowerconverters,andearly

definitionofenabledhumanexplorationsystemsandmissions(ex.MegawattElectricPropulsion,Moon/Mars

SurfacePower).Subsequentconverterdevelopmentwillimprovereadinessandlifetime,leadingto“flightready”

articles.AnintermediateNASAinfusionstepwoulddemonstratekilowatt-classnuclearpowersystemsapplicableto

MoonorMarssurface.HumanvehiclesystemdevelopmentwouldthenintegratetheseconverterswithDOE

nuclearreactortechnology,NASAbalanceofplant(ex.radiators,PMAD),andelectricpropulsion(ex.Q-thrusters,

VASIMR,Hallthrusters)todevelopan“ultimate”NASAapplicationofaHumanMarsMegawatt-classNuclear

ElectricPropulsionvehicleandmission.Terrestrialapplicationswouldbeinformed/infusedresultinginhigh

efficiencypowersystemswithgreatlyreducedcomplexityandcost.

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Solid-StateThermionicNuclearPowerForMegawattPropulsion,PlanetarySurfaceAndCommercialPowerProject

TECHNOLOGYDETAILS

AtStart:2 Current:2 AtEnd:4

1 2 3 4 5 6 7 8 9

AppliedResearch

Development Demo&Test

Solid-StateThermionic

NuclearPowerfor

MegawattPropulsion,

PlanetarySurfaceand

CommercialPower

TechnologyMaturity

ProjectDevelopmentPhases(3Years)

YearOne:Concepts,Missions,NanomaterialsEmission,LabConverterDemo.

Multi-MegawattNEPsystem&Marsmissionconcepts,modelsandanalysis.

Research&designofpracticalThermionicConverters.

Fabricatenanostructuredthermionicemittersofvarioussurfacesize&features.

Test&characterizethermionicemissionforvariousnanomaterials.

Examples:Tungsten,BaOcoated,alignedcarbonnanotubes,

nanocrystallinediamond

Demonstratethermionicpowerconversioninalaboratoryconfiguration.

Assess“modern”potentialtoincreaseefficiency,reduceoperationalemission

temperature,increasepowerdensity.

ExploreapplicabilitytosmallerpowersystemsfordeepspaceorMoon/Mars

surface,aswellaspotentialforsimpler,morecosteffectiveterrestrialnuclear

powerplants.

YearTwo:BreadboardConverterDDT&E.

YearThree:BrassboardConverterDDT&E

Thistechnologyiscategorizedasahardwaresystemformannedspaceflight

TechnologyArea

TA03SpacePower&Energy...

PerformanceMetrics

Metric Unit Quantity

PowerConversionEfficiency(atMaturity) % 20

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Solid-StateThermionicNuclearPowerForMegawattPropulsion,PlanetarySurfaceAndCommercialPowerProject

TECHNOLOGYDETAILS

TECHNOLOGYDESCRIPTION(CONT'D)Storage(Primary)

TA02In-SpacePropulsionTechnologies(Secondary)

CAPABILITIESPROVIDEDThermionicconvertershaveaveryhighpotentialforDualUse.Commercialpowerplants,nuclearorotherwise,

wouldbenefitfromhighefficiencypowerconversionwithreducedplantcomplexity,maintenanceandcapitalcosts.

AnuclearplantbaseduponThermionicconversionmaybewellsuitedtomeetingDepartmentofEnergy(DOE)

goalsforitsnext-generationSmallModularReactorprogram.Atsmallerscales,successfulloweringoftheelectron

emissionthresholdwouldalsoallowThermionicconverterstoperformpowerscavengingorbottomingfrom

otherwise“wasteheat”.ThermionicswoulddoubletheefficiencyandrecoveryofThermoelectric“tailpipe”

convertersbeingdevelopedtoharnessautomotiveexhaustenergy,replacingelectricalalternatorsandeliminating

theirparasiticdragontheengine.

POTENTIALAPPLICATIONS1.SpaceNuclearPowerSystems

2.SpaceSolarPowerSystems

3.TerrestrialCommercialNuclearPowerPlants

4.TerrestrialCommercialFossilFuelPowerPlants

5.TerrestrialSolarPowerPlants

6.AutomobileWasteHeat"Scavenging"

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Solid-StateThermionicNuclearPowerForMegawattPropulsion,PlanetarySurfaceAndCommercialPowerProject

IMAGEGALLERY

NASA/JSCPropulsionandPowerDivision

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Solid-StateThermionicNuclearPowerForMegawattPropulsion,PlanetarySurfaceAndCommercialPowerProject

ABSTRACT(CONTINUEDFROMPAGE1)

Forexample,two“small”(6kWe)ThermionicSpaceReactorswereflownbytheUSSRin1987-88foroceanradar

reconnaissance.HigherpoweredNuclear-ThermionicpowersystemsdrivingElectricPropulsion(Q-thruster,

VASIMR,etc.)mayofferthebreakthroughnecessaryforhumanMarsmissionsof<1yrroundtrip.Power

generationonEarthcouldbenefitfromsimpler,moeeconomicalnuclearplants,and"topping"ofmorefueland

emissionefficientfossil-fuelplants.

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Solid-StateThermionicNuclearPowerForMegawattPropulsion,PlanetarySurfaceAndCommercialPowerProject

ANTICIPATEDBENEFITS

ToNASAunfunded&plannedmissions:(CONT'D)couldenableHumanMarsmissionsof<1yearroundtripbyaffordingasystemofmegawattpower,lowspecific

mass(<10kg/kWe),greatlyreducedplantcomplexity,andassociatedsavingsindevelopmentcost.

AdvancedNuclear-ThermionicpowersystemsdrivingElectricPropulsion(Q-thruster,VASIMR,Hall,Ion,MPD,etc.)

mayofferthebreakthroughnecessaryforhumanMarsmissionsof<1yearroundtrip,resultinginsignificant

improvementtocrewhealthandsafety,largereductionsinconsumablesmass,massofsparesandredundancy,

andreduced"window"forcatastrophichardwarefailureorsolarflareevents.

Toothergovernmentagencies:TheDepartmentofEnergy(DOE)SmallModularReactor(SMR)Programmaybenefitfromthisworkintheareaof

efficientandeconomicalcommercialnuclearpowerplantswithfewerparts,fluidloops,andwasteproducts.

Tothenation:Terrestrialapplicationswouldbeinformedandinfusedresultinginhighefficiencypowersystemswithgreatly

reducedcomplexityandcost.Benefitsincludehighconversionefficiency(20%),staticoperationwithnomoving

partsandpotentialforhighreliability,greatlyreducedplantcomplexity,andpotentialforlowerDesign,

Development,TestandEvaluation(DDT&E)costs.Thiscouldleadtomoreefficientandeconomicalnuclearpower

plants,oralternativelyserveasa"topping"cycleinfossilfuelplantstoreducefuelconsumption,emissionsand

cost.Solarpowerplantsmaybecomeamorecompetitiveoption.Automobilesandbusesmayconsumelessfuel

andproducelasswastegasbyscavengingwasteheatfromengineblocksandexhaust.

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