NAUTILUS-X Future in Space Operations (FISO) Group Presentation

Technology Applications Assessment Team T A A T N on – A tmospheric U niversal T ransport I ntended for L engthy U nited S tates - - - - - - - - - - X- ploration M.L. Holderman JSC/SSP Multi-Mission Space Exploration Vehicle [email_address] NAUTILUS - X

Description and Objectives: Justification: Approach: Collaborators/Roles: ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],COST: $ 3.7 B DCT & Implementation 64 months ,[object Object],[object Object],[object Object],[object Object],[object Object],M.L. Holderman JSC/SSP N on – A tmospheric U niversal T ransport I ntended for L engthy U nited S tates - - - - - - - X- ploration Technology Applications Assessment Team T A A T

Technology Applications Assessment Team T A A T ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Multi-Mission Space Exploration Vehicle M.L. Holderman JSC/SSP System Goals NAUTILUS - X

T A A T Technology Applications Assessment Team Multi-Mission Space Exploration Vehicle ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],M.L. Holderman JSC/SSP Attributes NAUTILUS - X

Technology Applications Assessment Team T A A T M.L. Holderman JSC/SSP Multi-Mission Space Exploration Vehicle ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Attributes NAUTILUS - X

T A A T Technology Applications Assessment Team Multi-Mission Space Exploration Vehicle Technology Development ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],M.L. Holderman JSC/SSP NAUTILUS - X

Technology Applications Assessment Team T A A T M.L. Holderman JSC/SSP ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Technology Development Multi-Mission Space Exploration Vehicle NAUTILUS - X

M.L. Holderman JSC/SSP Technology Applications Assessment Team T A A T Industrial Airlock slide-out Unit Command/Control & Observation Deck Multi-Mission Space Exploration Vehicle Orion & Commercial Docking Port PV Array deployed: Core Module - 6.5m - 14m Full Operational Status: CIS-Lunar & NEO Mission NAUTILUS - X

M.L. Holderman JSC/SSP Technology Applications Assessment Team T A A T Multi-Mission Space Exploration Vehicle External “ Dynamic ” Ring-flywheel Start-up Thrusters Hoberman Circumferential Stabilizing Ring(s) Soft-wall Inflatable section(s) Completed Centrifuge w/ External Flywheel NAUTILUS - X

M.L. Holderman JSC/SSP Technology Applications Assessment Team T A A T Multi-Mission Space Exploration Vehicle View looking “Forward” NAUTILUS - X

Description and Objectives: Justification : Approach: Collaborators/Roles: ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],JSC: Design Requirements/Project Mngt., Centrifuge Design/Test, Instrumentation, Control Avionics/SW, Deployment scheme, Structural Design & Materials selection, Crew Training, On-Orbit Test OPS JSC/Ames: Hub Seal & Bearings, Payload Integration Draper Labs: ISS G N&C impacts GRC: Flywheel Design/Integr. LaRC: Hoberman alignment & load Cirlce ,[object Object],[object Object],[object Object],[object Object],[object Object],T A A T Technology Applications Assessment Team Mark L. Holderman JSC/SSP ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Multi-Mission Space Exploration Vehicle Technology Applications Assessment Team T A A T Development Challenges ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Multi-Mission Space Exploration Vehicle Technology Applications Assessment Team T A A T M.L. Holderman JSC/SSP Partnering & Collaboration ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

T A A T Technology Applications Assessment Team Multi-Mission Space Exploration Vehicle Technology Development M.L. Holderman JSC/SSP ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],First TAAT Demonstration NAUTILUS - X

Multi-Mission Space Exploration Vehicle T A A T Technology Applications Assessment Team ,[object Object],[object Object],[object Object],[object Object],2011-2013 DEMO COST: $84M - $143M Mark L. Holderman JSC/SSP

[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],T A A T Technology Applications Assessment Team Mark L. Holderman JSC/SSP DEMO Aspects: ,[object Object],[object Object],[object Object],Partial - (g) RPM 30ft dia. 40ft dia. 4 .08 .11 5 .13 .17 6 .18 .25 7 .25 .33 8 .33 .44 9 .41 .55 10 .51 . 69 SRMS in Berth-mode while Orbiter Air-lock is placed in Soft-Dock during micro-(g) activities on ISS

COST: $84-143M DCT & Implement <39 months Design, Construct, Test & Implement: DCT&I T A A T Technology Applications Assessment Team Mark L. Holderman JSC/SSP http://www.hoberman.com/portfolio/hobermansphere-lsc.php?myNum=10&mytext=Hoberman+Sphere+%28New+Jersey%29&myrollovertext=%3Cu%3EHoberman+Sphere+%28New+Jersey%29%3C%2Fu%3E&category=&projectname=Hoberman+Sphere+%28New+Jersey%29 * Test & Evaluation Centrifuge designed with capability to become Sleep Module for Crew Hoberman Circular Deployment & Load outer ring Nested jacking cylinders for Transit Tunnel ex-Orbiter External AirLock Dynamic external Ring-Flywheel Astromast w/ Hard-node Stabilizer Rings Inner Jack-knife Stabilizer Soft-Berth mechanism [internal]: Micro-(g) mitigation Internal Ballast Bladders

[object Object],[object Object],[object Object],[object Object],Technology Applications Assessment Team T A A T Mark L. Holderman JSC/SSP ,[object Object],[object Object],[object Object],[object Object],DEMO Aspects: * Test & Evaluation Centrifuge designed with capability to become Sleep Module for Crew ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Mark L. Holderman JSC/SSP Technology Applications Assessment Team T A A T ,[object Object],[object Object],[object Object],[object Object]

[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Technology Applications Assessment Team T A A T Mark L. Holderman JSC/SSP

Technology Applications Assessment Team Mark L. Holderman JSC/SSP T A A T ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Technology Applications Assessment Team T A A T Back-Up Charts

Solar Electric Propulsion Spin out L1 MMSEV DEPOT Life Boat/Living Quarters Staging location/Hospital Waiting for engines to go to MARS INSITU (ICE, water) Lunar Exploration Crew Transfer Technology Applications Assessment Team M.L. Holderman JSC/SSP Multi-Mission Space Exploration Vehicle Initial Operation(s) Concept T A A T NAUTILUS - X

Technology Applications Assessment Team T A A T M.L. Holderman JSC/SSP Multi-Mission Space Exploration Vehicle NAUTILUS - X

Centrifuge Command /Control Deck & Manipulator Station Air-Lock w/ staging platform ,[object Object],[object Object],[object Object],Solar Array ,[object Object],[object Object],[object Object],[object Object],[object Object],Communications Array Attitude Control & CMG cluster Docking Port (Orion, Commercial, Int’l) Technology Applications Assessment Team T A A T Multi-Mission Space Exploration Vehicle Radiation Mitigation Chamber M.L. Holderman JSC/SSP NAUTILUS - X

M.L. Holderman JSC/SSP Folding PV arrays Decent Vehicle Hangar Primary Communications Dish Propulsion ECLSS Module Adaptable full-span RMS Command/Observation Deck Primary Docking Port Logistical Stores Centrifuge Radiation Mitigation Extended Duration Explorer Technology Applications Assessment Team Multi-Mission Space Exploration Vehicle Science Probe Craft & Mini Service-EVA-Pods

Technology Applications Assessment Team M.L. Holderman JSC/SSP T A A T Multi-Mission Space Exploration Vehicle Extended Duration Explorer NAUTILUS - X

NAUTILUS-X Future in Space Operations (FISO) Group Presentation

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NAUTILUS-X Future in Space Operations (FISO) Group Presentation