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![Page 1: March 19, 2007S. A. Getty NASA Headquarters ESMD Faculty-Student Research Team: Nanotechnology for Exploration and Science Dr. Stephanie A. Getty NASA.](https://reader036.fdocuments.us/reader036/viewer/2022062409/56649d3f5503460f94a196b2/html5/thumbnails/1.jpg)
March 19, 2007 S. A. Getty NASA Headquarters
ESMD Faculty-Student Research Team: ESMD Faculty-Student Research Team: Nanotechnology for Exploration and ScienceNanotechnology for Exploration and Science
Dr. Stephanie A. GettyNASA GSFCCode 541
Materials Engineering Branch
Applied Nanotechnology
Prof. David D. AllredBrigham Young University
Dept. of Physics and AstronomyStudents: Jonathon Brame
Johnathan Goodsell
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March 19, 2007 S. A. Getty NASA Headquarters
NASA’s Exploration InitiativeNASA’s Exploration InitiativeCourtesy NASA website
To the Moon, Mars and Beyond
The Vision for Space Exploration calls for humans to return to the moon by the end of the next decade, paving the way for eventual journeys to Mars and beyond.
Courtesy NASA website
To the Moon, Mars and Beyond
The Vision for Space Exploration calls for humans to return to the moon by the end of the next decade, paving the way for eventual journeys to Mars and beyond.
Carbon Nanotube- Magnetic analysis of geological based Magnetometer : samples on Mars and the Moon
Orientation for manned expeditionsLocation of mining resources
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March 19, 2007 S. A. Getty NASA Headquarters
Projects ongoing in GSFC NanoDevices GroupProjects ongoing in GSFC NanoDevices Group
– Strain-based NanoCompass• GSFC: 541, 691 • BYU summer intern team: Prof. D. Allred, Johnathan
Goodsell, Jon Brame
– Electron gun for miniaturized mass spectrometer• GSFC: 541, 553, 699 • Fisk University summer intern: Melissa Harrison
– Generalized strain sensors• GSFC: 541, 660 • BYU summer intern team: Prof. D. Allred, Johnathan
Goodsell, Jon Brame• Fisk University summer intern: Melissa Harrison
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March 19, 2007 S. A. Getty NASA Headquarters
Background Information:Background Information:Carbon NanotubesCarbon Nanotubes
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March 19, 2007 S. A. Getty NASA Headquarters
Nanoelectronic MaterialsNanoelectronic MaterialsSingle-walled Carbon
Nanotubes
• Metallic or Semiconducting– Difficult to control trend toward
SWCNT network devices
• Electronic properties sensitive to deformation– Strain sensing
Courtesy Smalley Group, Rice Univ.
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March 19, 2007 S. A. Getty NASA Headquarters
Vapor-Liquid-Solid GrowthVapor-Liquid-Solid GrowthFeedstock gas liquid alloy solid nanostructure
SWCNTs:•Catalyst = Fe(NO3)3:IPA or thin film Fe•Feedstock = CH4 and C2H4
•TG = 950°C, tG = 5-10 minutes
MWCNTs:•Catalyst = thin film Al/Fe bilayer•Feedstock = C2H4
•TG = 750°C, tG = 5-10 minutes
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March 19, 2007 S. A. Getty NASA Headquarters
Thin Film Fe CatalystThin Film Fe Catalyst
• High density
• Improved cleanliness
20 nm
TEM studies show–SWCNTs –MWCNTs–bundles
TG = 950°C
NanoCompass
Johnathan Goodsell, Prof. David Allred, Prof. R. Vanfleet (BYU)
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March 19, 2007 S. A. Getty NASA Headquarters
Summary of Progress: SWCNT GrowthSummary of Progress: SWCNT Growth
• Johnathan Goodsell – Brigham Young University– Mechanical Engineering Major
• Summer project: Optimize growth of SWCNTs using thin film catalyst– New process for GSFC– Crucial for NanoCompass development
• Excellent results in only 8 weeks – Contributed to IEEE Nano 2006 Presentation,
Cincinnati, OH, July 2006
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March 19, 2007 S. A. Getty NASA Headquarters
SWCNT NanoCompass for High SWCNT NanoCompass for High Spatial Resolution MagnetometrySpatial Resolution Magnetometry
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March 19, 2007 S. A. Getty NASA Headquarters
Applications:• Magnetospheric Science• Spacecraft Orientation• Planetary Geomagnetism
but• cm-scale resolution• Limited materials supply
Fluxgate Magnetometer:• High sensitivity (nTesla)• Low noise
M. H. Acuna, Rev. Sci. Inst. 73, 3717 (2002)
Technological MotivationTechnological MotivationMars
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March 19, 2007 S. A. Getty NASA Headquarters
NanoCompass DesignNanoCompass Design
● Au Electrodes
Single-Walled Carbon Nanotubes ● Ferromagnetic Needle Mech coupled to SWCNTs Deflected in Magnetic Field
NanoCompass
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March 19, 2007 S. A. Getty NASA Headquarters
Projected SpecificationsProjected Specifications
NanoCompass (estimated)
UCLA fluxgate (ST5)
Max Op Temp ~450°C 100°C
Sensor Dimensions
10-5 cm x 10-5 cm on Si (scalable)
4 cm x 4 cm x 6 cm
Sensor [Array] Mass
1 g 75 g
Sensor Op Power 10-3 - 10-2 mW 50 mW
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March 19, 2007 S. A. Getty NASA Headquarters
NanoCompass Fabrication (to step 4)NanoCompass Fabrication (to step 4)
Materials can be robust to fabrication process
Next steps:• Reduce electrode
spacing• Reduce needle width• Increase trench depth
NanoCompass
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March 19, 2007 S. A. Getty NASA Headquarters
Future Work: Variability in ProcessingFuture Work: Variability in Processing
• SWCNT device electrically intact
• During magnetic field testing, continuity lost
• Next prototype in progress
Au
Au
SWCNTs
Remnantneedle
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March 19, 2007 S. A. Getty NASA Headquarters
Generalized Strain Sensing Generalized Strain Sensing Using SWCNTsUsing SWCNTs
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March 19, 2007 S. A. Getty NASA Headquarters
Flexible substratesFlexible substrates• Parylene, PDMS are candidates
– Modular electromechanical strain sensors– Modular field emitters– Application-adaptive devices
• Parylene: vapor-phase coated polymer, highly chemically resistant, excellent electronic insulator
• PDMS: polydimethylsiloxane, two-part curable elastomer, chemically resistant, good electronic insulator – to be demonstrated in SWCNTs
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March 19, 2007 S. A. Getty NASA Headquarters
Device Transfer to ParyleneDevice Transfer to Parylene
O2 plasma 3. Transfer to PDMS by substrate removal
1. Fabricate SWCNT device on rigid substrate to allow electrical characterization
Wet etch
2. Deposit parylene
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March 19, 2007 S. A. Getty NASA Headquarters
Parylene-bound SWCNT Strain DeviceParylene-bound SWCNT Strain DeviceFlexible Substrates
Jonathon Brame, Prof. David Allred (BYU)
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March 19, 2007 S. A. Getty NASA Headquarters
Preliminary ResultsPreliminary Results
• Large increase in device resistance with application of strain, as expected
• Need to separate contact effects from piezoresistive effects
• Need to evaluate reproducibility
The slope of the lines between 4µm stretch sets indicates that the resistance increases reversibly with increased strain.
Flexible Substrates
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March 19, 2007 S. A. Getty NASA Headquarters
Summary of Progress: Parylene-bound SWCNT Summary of Progress: Parylene-bound SWCNT DevicesDevices
• Jonathon Brame – Brigham Young University– Physics Major
• Summer project:– Demonstrate transfer of SWCNTs to parylene substrates– Test electromechanical response
• Preliminary fabrication and test completed in only 12 weeks – Publication and presentation at MRS Fall Meeting, Boston,
November 2006– “Strain-based Electrical Properties of Systems of Carbon
Nanotubes Embedded in Parylene,” Jon Brame, Stephanie Getty, Johnathan Goodsell, and David Dean Allred, Proceedings, Materials Research Society Fall 2006 Meeting.
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March 19, 2007 S. A. Getty NASA Headquarters
Status of Collaboration: GSFC-BYU TeamStatus of Collaboration: GSFC-BYU Team
• BYU Team has major role in Mars Desert Research Station (UT) – In situ demonstration of NanoCompass operation– Student-operated for outreach effort– Relevant to manned missions to the Moon and Mars
• Joint proposal submitted to support NanoCompass:– ROSES Planetary Instrument Definition and Development– Decision Pending
• Building growth/characterization facility at BYU– Correlated results, independent of location, important to the
CNT field– Measurements of CNT response in extreme UV planned– Possible applications in nanomaterial sensing for workplace
safety monitoring
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March 19, 2007 S. A. Getty NASA Headquarters
AcknowledgementsAcknowledgements• Dr. Peter Wasilewski GSFC/Astrochemistry Laboratory
• Dr. Louis Barbier GSFC/Exploration of the Universe Division
• Dr. Paul Mahaffy GSFC/Atmospheric Experiments Laboratory
• Patrick Roman GSFC/Detector Systems Branch
• Barney Lynch GSFC/Detector Systems Branch
• Dr. Federico Herrero GSFC/Detector Systems Branch
• Rusty Jones GSFC/Detector Systems Branch
• Dr. Todd King GSFC/Materials Engineering Branch
• Rachael Bis GSFC/Materials Engineering Branch
• Michael Beamesderfer GSFC/Materials Engineering Branch
• Lance Delzeit ARC/Nanotechnology Branch
• Prof. Gunther Kletetschka GSFC/Catholic University of America
• Vilem Mikula GSFC/Catholic University of America
• Tomoko Adachi GSFC/Catholic University of AmericaESMD Summer Internship Program
• Prof. David Allred Brigham Young University/Dept. of Physics & Astronomy
• Prof. Richard Vanfleet Brigham Young University/Dept. of Physics & Astronomy
• Johnathan Goodsell Brigham Young University/Mechanical Engineering Dept.
• Jonathon Brame Brigham Young University/Dept. of Physics & Astronomy MUCERPI Summer Internship Program
• Melissa Harrison Fisk UniversityThis work was supported by the Goddard Space Flight Center Director’s Discretionary Fund, the GSFC IRAD Program,
the Minority University College Education and Research Partnership Initiative, and the Exploration Systems Mission Directorate Faculty-Student Summer Internship Program
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March 19, 2007 S. A. Getty NASA Headquarters
Extra SlidesExtra Slides
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March 19, 2007 S. A. Getty NASA Headquarters
Nanoelectronic MaterialsNanoelectronic MaterialsSingle-walled Carbon Nanotubes
• Characterized by chirality, diameter– Diameter ~ 1 nm
• Metallic or Semiconducting– Difficult to control trend toward
SWCNT network devices
• Electronic properties sensitive to deformation– Strain sensing Courtesy Smalley Group, Rice Univ.
Courtesy Fuhrer Group, Univ Maryland, College Park
Metallic SWCNT:
n – m = 3 x integer
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March 19, 2007 S. A. Getty NASA Headquarters
Nanoelectronic Materials, Cont.Nanoelectronic Materials, Cont.Multi-walled Carbon Nanotubes
• Exclusively metallic– Similar to graphite
• Diameters 30-100 nm– Larger than SWCNTs
• High aspect ratio with many
available electrons– Field emission
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March 19, 2007 S. A. Getty NASA Headquarters
E-gun for MEMS Time-of-Flight Planetary Atmospheric ScienceMass Spectrometer : and biologically significant
molecular species for astrobiology
Ion lens assembly prototype
Carbon Nanotube-based Electron Gun
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March 19, 2007 S. A. Getty NASA Headquarters
Comparison: Candidate TechnologiesComparison: Candidate Technologies
MWCNTs
Spindt Emitters
Thermionic
Type
MetricCNT Field
EmitterSpindt
EmitterThermionic
Emitter
Density 1010 /cm2* 5x107 /cm2† 1 /cm2
Current @ Voltage
100μA @ 50V**1mA @
150 V*
Operating Temp
Ambient Ambient >700°C¶
Redundancy (2mm diam)
3x108 106 1
*This work **Optimized†V. M. Aguero and R. C. Adamo, 6th Spacecraft Charging Technology Conference (2000).¶Barium Oxide-coated Tungsten
Field Emission
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March 19, 2007 S. A. Getty NASA Headquarters
• CNT tower dimensions – 5 μm x 5 μm x
10 μm (height)
• 50 μm pitch• 2mm x 2mm
array
Field Emission
Patterned CNT CathodePatterned CNT Cathode
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March 19, 2007 S. A. Getty NASA Headquarters
Patterned MWCNTs for High Patterned MWCNTs for High Performance E-gunPerformance E-gun
GSFC patterned MWCNT emitter:
• Cathode-grid spacing = 140 µm
• Turn-on voltage <100 V
• 50 µA @ 10 mW
Compare to Cassini-Huygens thermionic e-gun:
• 80 µA @ 1000 mW
Field Emission
-8 10-6
0
8 10-6
1.6 10-5
2.4 10-5
3.2 10-5
4 10-5
4.8 10-5
-2 10-12
0
2 10-12
4 10-12
6 10-12
8 10-12
1 10-11
1.2 10-11
0 50 100 150 200
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6
-Em
issi
on C
urr
ent
(A
)
-Em
ission C
urre
nt Den
sity (A/um
2)
Extraction Voltage (V; grid bias)
Electric Field (V/m)
0.6 0.7 0.8 0.9 1 1.1 1.2-30
-29
-28
-27
-26
-25
ln(J/E2)
1/E
Fit to Fowler-Nordheim Tunneling:
J = K1E2 exp(-K
2/E)
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March 19, 2007 S. A. Getty NASA Headquarters
-50
0.0
50
1.0 102
1.5 102
2.0 102
2.5 102
3.0 102
3.5 102
-50
0
50
100
150
200
250
300
350
-20 0 20 40 60 80 100 120 140
Turn-on voltage versus Cathode-Grid SpacingT
urn
-on
Vo
ltag
e (
V)
Cathode-Grid Spacing (um)
ARC1
GSFC060802-2GSFC060802-2
ARC2-21
ARC2-11
GSFC060803-1 GSFCpattern-1ARC2-22
GSFC:EGp2
Sample DatabaseSample Database
Best performer:– GSFC patterned
sample– 50 uA @ gap =
140 um
Field Emission
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March 19, 2007 S. A. Getty NASA Headquarters
Side-by-Side E-Gun EvaluationSide-by-Side E-Gun EvaluationField Emission
Recent and Upcoming Work:Compare candidate e-gun technologies, fully integrated with aperture/lens stack
lens stack
filament
repeller
Towards Integration into MEMS Time-of-Flight Mass Spectrometer
CNT e-gunThermionic e-gun
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March 19, 2007 S. A. Getty NASA Headquarters
Future Work for Summer Interns: CNT E-GunFuture Work for Summer Interns: CNT E-Gun
• Lifetime testing of CNT emitters• Study of performance in ambient gas
environment• Maturation of fabrication techniques• Maturation of packaging techniques• Advanced electronics to develop
feedback/ballast for current stabilization