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HSF Transition: ISS, LEO and beyond to cislunar space Sam Scimemi Director, International Space Station “Buona notte” Kelly at 180 days onboard the ISS March 2016

HSF Transition: ISS, LEO and beyond to cislunar space...Ø Visual impairment/intracranial pressure risk and assess countermeasures Ø Space radiaon protec0on/monitoring systems Ø

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Page 1: HSF Transition: ISS, LEO and beyond to cislunar space...Ø Visual impairment/intracranial pressure risk and assess countermeasures Ø Space radiaon protec0on/monitoring systems Ø

HSF Transition: ISS, LEO and beyond to cislunar space

Sam Scimemi Director, International Space Station

“Buona notte” Kelly at 180 days onboard the ISS

March 2016

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Strategic Principles for Sustainable Exploration

•  Implementable in the near-term with the buying power of current budgets and in the longer term with budgets commensurate with economic growth;

•  Exploration enables science and science enables exploration, leveraging robotic expertise for human exploration of the solar system

•  Application of high Technology Readiness Level (TRL) technologies for near term missions, while focusing sustained investments on technologies and capabilities to address challenges of future missions;

•  Near-term mission opportunities with a defined cadence of compelling and integrated human and robotic missions providing for an incremental buildup of capabilities for more complex missions over time;

•  Opportunities for U.S. commercial business to further enhance the experience and business base;

•  Resilient architecture featuring multi-use, evolvable space infrastructure, minimizing unique major developments, with each mission leaving something behind to support subsequent missions; and

•  Substantial new international and commercial partnerships, leveraging the current International Space Station partnership while building new cooperative ventures.

•  Continuity of human spaceflight is essential to sustain progress; we will establish a regular cadence of crewed missions to cislunar prior to the end of ISS .

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The Bigger Picture

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Near-term execution

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Planning the transition from ISS to cislunar space •  Instead of declaring a definite end date for ISS, NASA will focus on considerations

such as –  Short term crewed habitation missions are being executed in cis-lunar space while

ISS is still operational and being utilized –  Exploration research and technology/system development activities requiring ISS as

a testbed are essentially complete –  There is an expanded commercial market and broad private/government/academic

demand for LEO-based platforms that are based on private and/or public/private business models

–  Value benefit of the ISS has been sufficiently achieved –  Maximizing international ISS partnership and participation –  Safe sustainment of the ISS will remain paramount

•  Based on todays planning and reasonable progress towards our goals, transitioning HSF could be expected in the mid-2020s

–  NASA is working with stakeholders, International Partners and industry to develop plans for transitioning the ISS and the Partnership

–  The Partnership should explore possible outcomes for the ISS platform at its’ end-of-life

•  De-orbit, disassemble, turn over portions to private industry, maintain government ownership, others ideas

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Vision:Sustainedeconomicac0vityinLEOenabledbyhumanspaceflight,drivenbyprivateandpublicinvestmentscrea0ngvalueandbenefi?ngEarththroughcommercialsupplyandpublicandprivatedemand

•  User-friendlyISSprocessimprovements

•  Maximizethroughput

•  Demonstrate&communicatevalueproposi0onofISS

•  Foster“successstories”

•  U0lizemorecommercialacquisi0onstrategies

•  Establishinteragencyworkinggrouptoaddresspolicyandregulatoryissues

•  Inves0gateeconomicclusterpoten0al

•  AddressbarrierssuchasIPreten0on,liability,ITAR

•  LeverageNASANEXTStepsBAAstudiesandfollow-ontoenablecommercialLEOcapabili0es

•  EnableEarth-similarlaboratorycapabili0esforISSthatcantransi0ontocommercialplaVorms

•  Transi0onfromNASA-suppliedtocommercially-suppliedservicesandcapabili0esonceavailable

•  Establishconsor0aforpoten0alhigh-payoff,market-enablingmicrogravityandLEOapplica0onswithpublicandprivatefundstosupportdevelopment(e.g.proteincrystalliza0on,exo0cfibers,lightweightalloys,3D0ssues,earthobserving,etc)

•  EstablishcommercialLEO

u0liza0onuniversitycurriculumandprograms

NASA vision for LEO beyond ISS

1)LEOcommercializa0onenabledbyleveragingISS

2)Thepolicyandregulatoryenvironmentpromotescommercializa0onofLEO

3)Arobust,self-sustaining,andcosteffec0vesupplyofUScommercialservicesto/in/fromLEOaccommodatespublicandprivatedemands

4.0BroadsectorsoftheeconomyusingLEOforcommercialpurposesGO

ALS

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Endswithtes0ng,researchand

demoscomplete*

AsteroidRedirectCrewedMissionMarksMovefrom

Phase1toPhase2

EndswithoneyearcrewedMars-classshakedowncruise

Today

2030

Mid-2020s*Thereareseveralotherconsidera0onsforISSend-of-life

Transition framework from ISS to Cislunar Space

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Phase0:Explora0onSystemsTes$ngonISS

Phase1:CislunarFlightTes$ngofExplora0onSystems

Phase2:CislunarValida$onofExplora0onCapability

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Phase1:Cis-lunarFlightTes4ngofExplora4onSystems

§  DemonstratethatSLSandlaunch

processingsystemscaninsertbothOrionandco-manifestedpayloadsintocis-lunarspace

§  DemonstratethatOrionandmissionopera4onscanconductcrewedmissionsincis-lunarspaceatleastfor21days

§  DemonstrateMars-extensiblesystemsandmissionopera4onsthatreduceriskforfuturedeepspacemissions(withEVA)beyond21days

Draft - Top-Level Phase Objectives

Phase0:Explora4onResearchandSystemsTes4ngonISS

§  TestMars-capablehabita4on

systems–ECLS,environmentalmonitoring,crewhealthequipment,explora0ongenera0onEVAsuit,firedetec0on/suppression,radia0onmonitoring

§  Completehumanhealth&performanceresearchandriskreduc0onac0vi0es

§  Demonstrateexplora4onrelatedtechnologiesandopera4ons•  Autonomouscrewopera0ons•  Docking,proxops

Phase2:Cis-lunarValida4onofExplora4onCapability

§  ValidateMarsclasshabita4onandhabita0onsystemfunc0onalityandperformance

§  ValidateMarsclasshumanhealthandperformance

§  Validateopera0onalreadinesstoleaveEarth-Moonsystemviaoneyear+“shakedowncruise”(noresupply/crewexchanges,limitedgroundinterac0on,etc.)

§  Validatecis-lunarasstagingorbits§  UseofhighpowerSEPfordeepspace

missions§  Asteroidrelatedoriginsofthesolar

systemscienceobjec0ves§  Demonstratereal-0merobo0clunar

surfaceac0vi0es§  Insituresourceu0liza0ondemonstra0ons

§  Robo0cmanipula0ontechnologyandtechniquesdemonstra0ons

§  Remotepresencetechnologydevelopmentanddemonstra0ons

§  Earth/spacescience§  EnabledevelopmentofLEOcommercial

market

•  Originsoftheuniverse,lunarrovervola0lesamplereturn

•  Otherscien0ficorresearchobjec0ves?

enables enables enables

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Phase 0 Research and Technology Development that feeds forward to the Proving ground

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Habitation Systems Goals

System Includes Today Mars Goal

Life Support

Air revitalization, water recovery, waste collection

and processing

42% recovery of O2 from CO2; 90% recovery of H2O; <6 mo MTBF for some

components

>75% recovery of O2 from CO2; >98% recovery of H2O;

>2 yr MTBF

Environmental Monitoring

atmosphere, water, microbial, particulate, and acoustic

monitors

Limited, crew-intensive on-board capability; rely on sample return

to Earth

On-board analysis capability with no sample return; identify and quantify

species and organisms in air & water

Crew Health

exercise equipment, medical treatment and diagnostic equipment, long-duration

food storage

Large, cumbersome exercise equipment, limited on-orbit

medical capability, food system based on frequent resupply

Small, effective exercise equipment, on-board medical capabilities, long-

duration food system

EVA Exploration suit ISS EMU’s based on Shuttle

heritage technology; not extensible to surface ops

Next generation spacesuit with greater mobility, reliability, enhanced life

support, operational flexibility

Fire

Non-toxic portable fire extinguisher, emergency

mask, combustion products monitor, fire cleanup device

Large CO2 suppressant tanks, 2-cartridge mask, obsolete fire

products. No fire cleanup other than depress/repress

Unified fire safety approach that works across small and large architecture

elements

Radiation Protection

Low atomic number materials including polyethylene, water, or any hydrogen-containing

materials

Node 2 CQ’s augmented with polyethylene to reduce the impacts of trapped proton

irradiation for ISS crew members

Solar particle event storm shelter based on optimized position of on-

board materials and CQ’s with minimized upmass to eliminate major impact of solar particle event on total

mission dose 10

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Human Health and Performance Research Transition from ISS to Cis-Lunar Space

ISSGoalsforSpaceExplora4on(inves4gate,develop,andtest)

Ø Humanhealthrisksandcapabili0estomi0gatetheserisks

Ø Explora0onbiomedicaltechnologiesandtools

Ø Extendmissiondura0onstoone-yeartotestsix-monthresearchandcountermeasures

Ø Visualimpairment/intracranialpressureriskandassesscountermeasures

Ø Spaceradia0onprotec0on/monitoringsystems

Ø Long-dura0onspaceflightstressorstotheimmunesystemandmicrobiome

Ø Explora0onfoodsystemtechnologies

Ø Crewhabita0onstandardsandmodels

MarsGoalsforCis-lunarSpace(validate)

Ø  Advancedcountermeasuresagainstdecondi0oning(bone,muscle,cardiovascular)

Ø  Crewperformance,psychologicalwell-being,

andinterven0onforMarsflightopera0onsØ  Integratedmedicalcapabili0es(autonomous

medicaldiagnosisandtreatment)

Ø  HumanandenvironmentalhealthinaclosedMarsspacecrah(immunesystem,microbiome)

Ø  Marsmissionfoodsystem

Ø  Spaceradia0onprotec0on/monitoringsystems

Ø  Crewhabita0onsystems(humancomputer/robo0c/vehicleinterfaces)

Ø  Robustness/reliabilityofcrewexercisesystems11

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Next slides will focus on a discussion of Phase 1 objectives

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Draft - Cis-lunar Flight Testing of Exploration Systems

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Phase1:CislunarFlightTes$ngofExplora0onSystemsAsteroidRetrievalCrewedMissionMarksMovefrom

Phase1toPhase2

Considera0ons,Constraints,andUnknowns:

-  Ini0almissiondesigndrivenbyneedtomeetflighttestobjec0ves

MISSIONELEMENTSANDCAPABILITIES:

•  SLSBlock1(EM-1)•  Orion•  SecondaryPayloaddeployment

OBJECTIVES:

•  DemonstrateintegratedSLS/Orioncapabilityfromlaunchthroughrecoveryincis-lunarspace

•  Obtainascentandin-spaceenvironmentsdata•  Demonstrateperformanceofcommunica0ons,network,and

trackingcapabili0es•  Demonstrategroundprocessingandopera0onalsupport•  Deploysecondarypayloads

EM-1

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Draft - Cis-lunar Flight Testing of Exploration Systems

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Phase1:CislunarFlightTes$ngofExplora0onSystemsAsteroidRetrievalCrewedMissionMarksMovefrom

Phase1toPhase2

Considera0ons,Constraints,andUnknowns:

-  Ini0almissiondesigndrivenbyneedtomeetflighttestobjec0ves

-  Ini0alco-manifes0ngplanningdrivenbyconserva0veanalysis

-  Proximityopera0onsunderevalua0on

MISSIONELEMENTSANDCAPABILITIES:

•  SLSBlock1B(EM-2andsubsequent)•  Orion•  Co-manifestedcapability(inwork)

OBJECTIVES:

•  DemonstrateSLS/Orioncrewedcislunartransporta0onandtrajectorycapabilityincislunarspaceupto21daysw/4crew

•  Demonstrateco-manifestedpayloadcapabilityincis-lunarspace(~5MTorbeker)

EM-2

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Draft - Cis-lunar Flight Testing of Exploration Systems

15

Phase1:CislunarFlightTes$ngofExplora0onSystemsAsteroidRedirectCrewedMissionMarksMovefrom

Phase1toPhase2

Considera0ons,Constraints,andUnknowns:

- Mission(s)orbitdrivenbyARCMmissionobjec0ves

-  Co-manifes0ngcapabilityunderanalysis

-  Partnerdiscussionscon0nueonexecu0onofARMandARCMmissionsandco-manifestedelements

- Numberofaddi0onalmissionsrequiredtoexecuteARCMdependentonriskbuy-downofpreviousmissionsandeventualco-manifes0ngcapability

MISSIONELEMENTSANDCAPABILITIES:

•  SLSBlock1B•  Orion•  Co-manifestedelement(s)withdocking,power,propulsionand

missionaugmenta0oncapabili0estosupportincreasinglyambi0ousmissionsinPhase2

•  (ARMrobo0cspacecrah)

OBJECTIVES:

•  Demonstrateextendedcrewedopera0onsincis-lunarspacewith4crewbeyond21days

•  Demonstra0onofcrewhealthandperformancesystemspar0cularlyexercise,medical,andradia0onprotec0on

•  DemonstratedeepspaceEVAcapability•  Deployco-manifestedelement(s)incislunarspace•  PerformARCMmissionobjec0ves

EM-Next 2-3

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Discussion

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