nanofoil – novel use for exploration of mars · 2017. 6. 2. · self propagating high temperature...

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Jacques Matteau Global Sales Manager [email protected] indium.us/F014 NanoFoil – Novel use for Exploration of Mars

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  • Jacques MatteauGlobal Sales Manager

    [email protected]

    indium.us/F014

    NanoFoil – Novel use for Exploration of Mars

  • NanoFoilA Reactive Multilayer Foil

    2 INDIUM CORPORATION CONFIDENTIAL

    Chemistries

    Heats

    Velocities

    Ignition

  • Reactive Materials

    3 INDIUM CORPORATION CONFIDENTIAL

    Reaction Product

    Heat of

    Reaction (kJ/mol)

    Adiabatic

    Temperature (°C)

    Phase of Product

    TiB2 -108 2920 solid & liquid ZrB2 -108 3000 solid & liquid HfB2 -110 3370 solid & liquid

    TiC -93 3067 solid & liquid ZrC -104 3417 solid & liquid HfC -105 3830 solid & liquid

    Ti5Si3 -72 2120 solid & liquid Zr5Si3 -72 2250 solid & liquid Nb5Si3 -57 2060 solid

    NiAl -59 1639 solid & liquid ZrAl -45 1480 solid & liquid PdAl -92 2380 liquid

  • Heats of Reaction and Maximum Reaction Temperatures

    4 INDIUM CORPORATION CONFIDENTIAL

    • Formation reactions: Ni/Al, Ti/C, Zr/Si, etc.– ∆Hrxn= 30 to 100 kJ/mol-atom

    – Tmax = 10000C to 30000C

    • Thermite Reactions: Al/CuOx, Al/FeOx, etc.– ∆Hrxn = 100 to 150 kJ/mole-atom

    – Tmax = 20000C to 40000C

    SHSSelf Propagating High Temperature Synthesis Reactions

  • NanoFoil Fabrication

    5 INDIUM CORPORATION CONFIDENTIAL

    • Magnetron Sputter Deposited

    • Free-standing Foils (10-200µm thick)

    • Bilayer Thicknesses - 10 to 500nm

    • Use Ni and Al layers

    • Several 1000 layers

    Motor

    Rotating Carousel

    Sputter Guns

    Substrates

  • 6 INDIUM CORPORATION CONFIDENTIAL

    Modeling Reaction Self-Propagationand Ignition

    Inputw,4δ, ∆Ηrx

    Model Reaction

    PredictProperties

    Reacted Material

    Ignition

    A layers

    B layers

    Intermixed Regions

    As-deposited FoilReaction Zone

    x

    y

    Thermal Diffusion

    Ato

    mic

    Diff

    usi

    on

    Propagation Direction

    Intermixing(w)

    BilayerThickness

    (4δ)

    A layers

    B layers

    ReactionZone

    ReactedFoil

    Ignition

    As-deposited Foil

    Thermal Diffusion

    Ato

    mic

    D

    iffu

    sion

  • NanoFoil General Reaction Scheme

    7 INDIUM CORPORATION CONFIDENTIAL

    (A) Photo of the exothermic wave (A); (B) SEM picture of the quenched reaction front; (C) TEM pictures of the reaction zone; (D) dynamics of the thickness of:• Ni layer ( ∆), Al-rich layer ( □), and bilayer period ( ○), • I-initial structure, II – Ni dissolution, III – NiAl p recipitation; (E) schematic draw of the wave structure.

    The sequence of the process stages can be represent ed as follows:

    Ni(s) + Al(s) ® Ni(s) + Al(m); Ni(s) + Al(m) ® Ni(s) + AlNix(m); Ni(s) + AlNix(m) ® AlNi(s),

    At the first stage, the aluminum melts just above t he reaction front due to heat flow from the reaction zone. Melting of Al initiates partial dissolution of the Ni layers (stage 2) into Al melt until the saturati on concentration (x ~ 0,25 - 0,3) is reached. At the third stage, solid grains of the NiAl B2-phas e nucleate and grow. The characteristic feature of the process is that t he grains have different crystallographic orientations and are separated by liquid/amorphous interlayers. The existence of the liquid between the solid grain s allows Ni to dissolve into the melt by means of liquid-state diffusion, which is m uch faster than solid state diffusion across the intermetallic solid compound.

  • 8 INDIUM CORPORATION CONFIDENTIAL

    400

    600

    800

    1000

    1200

    1400

    0 50 100 150 200 250

    As-Deposited6 hrs @ 150°C

    Hea

    ts o

    f Rea

    ctio

    n (

    J/g

    )

    Bilayer Thickness (nm)

    As-depositedw = 1.2nmAnnealedw = 3.1nm

    He

    at o

    f Re

    act

    ion

    (J/g

    )

    Bilayer Thickness (nm)

    w

    (4δ)

    Measured Heats of Reaction

  • Reaction Velocities can be Controlled/Predicted

    9 INDIUM CORPORATION CONFIDENTIAL

    0

    2

    4

    6

    8

    10

    12

    0 50 100 150 200 250

    Experiments: As-depositedExperiments: 6hrs @ 150°CPredictions: 6hrs @ 150°CPredictions: As-deposited

    Rea

    ctio

    n V

    eloc

    ity (

    m/s

    )

    Multilayer Period (nm)

    As-depositedw = 1.2nm

    Annealedw = 3.1nm

    Annealing increases intermixing and slows the reaction

    Bilayer Thickness (nm)

    Re

    act

    ion

    Velo

    city

    (m

    /s)

    Al/Ni VaporDepositedNanoFoil® A.J. Gavens, et. al, JAP, 1255, 2000

  • 1 in.

    Above: NanoFoil®

    with LED board and componentsLeft: Freestanding NanoFoil®

    • Largest Manufactured Piece: 43.5” x 9”

    • Smallest Produced Size: .010”x .010”*

    • Cutting Methods– Laser– Chemical Milling– Stamping– Hand Cutting

    • Packaging– Tape and Reel– Waffle Pack– Freestanding

    * Can be cut smaller,

    NanoFoil® Forms

    10

  • Tin Plated NanoFoil®

    11

    • Tin acts as solder• no solder preforms or prewet needed

    • Works with standard board finishes

    • Immersion tin• ENIG• Immersion silver

    • Lead-free and lead-tin compatible

    • Thickness 5µm (0.0002”) to 0.0012” (30µm) per side

    NanoFoil®

    Tin

    Tin

    SEM image: 40µm NanoFoil + 4µm tin each side

  • • Several techniques are available, depending on joint geometry

    • Ignition methods should be optimized for each customer/application: – Electrical heating: good for automated

    assembly– Laser: suitable for automated assembly – Spark: good for manual assembly– Flame/torch: avoids electric charge– Induction: NanoFoil® need not be exposed– Mechanical: Special applications

    Ignition Methods

  • Before reaction During reaction

    Final Product:Al-Ni Intermetallic

    Ni

    AlNanoFoil®

    TEM of unreacted NanoFoil

    TEM of reacted NanoFoil

    1000ºC to 1600ºC

    NanoFoil® Reaction

    13

  • NanoFoilA Reactive Multilayer Foil

    14 INDIUM CORPORATION CONFIDENTIAL

    Process and Use

    Space –

    The Final Frontier

  • Mars 2020 Current Plan

    15 INDIUM CORPORATION CONFIDENTIAL

  • Timeline for Mission 2020

    16 INDIUM CORPORATION CONFIDENTIAL

  • Land the Rover

    17 INDIUM CORPORATION CONFIDENTIAL

    Cache, drill, arm -mounted instrument set, surface prep tool

  • Sample Mars

    18 INDIUM CORPORATION CONFIDENTIAL

  • Cache

    19 INDIUM CORPORATION CONFIDENTIAL

  • Orbital Sample

    20 INDIUM CORPORATION CONFIDENTIAL

  • Back To Earth

    21 INDIUM CORPORATION CONFIDENTIAL

  • Summary

    • External Orbital Sample sterilization

    – Coating sphere with NanoFoil

    – Igniting Nanofoil after retrieval from Mars

    – Key to mission– No terrestrial contaminants

    – No Martian contaminants

    – NanoFoil sterilization

    – Work in progress

    Maximize possibility of identification of Martian Biosignature(s) in samples

    22 INDIUM CORPORATION CONFIDENTIAL