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A D V A N C E D

M A T E R I A L S

&

P R O C E S S E S | F E B R U A R Y

2 0 1 6

2 1

Fig. 2 —

Field-assisted sintering units:

(a) 25 ton, (b) 250 ton, (c) hybrid 320 ton.

(a)

(b)

(c)

of a sub-micron grain microstructure;

achieving 100% density; and energy

savings of 60-70%. Applications range

from hypersonic vehicles and optical

mirrors to cutting tools and aerospace

components. The technology enables

engineering of new materials and

design and development of prototype

components with features not econom-

ically feasible using conventional man-

ufacturing methods.

THERMALLY MANAGED

COMPONENTS

Space exploration is one endeav-

or where thermal management is of

critical importance. For example, NASA

is seeking thrusters with double the

thrust-to-weight ratio using advanced

propulsion techniques such as the Nu-

clear Thermal Propulsion (NTP) system

shown in Fig. 3. Requirements for the

NTP rocket nozzle include high thermal

conductivity, good mechanical proper-

ties, and light weight.

The thermal conductivity of dia-

mond is three to six times higher than

that of copper, whereas thermally

grown pyrolitic (TGP) graphite is four

times higher (in plane). Similarly,

thermal conductivities of multiwall

carbon nanotubes (MWCNT) and sin-

gle wall carbon nanotubes (SWCNT)

are about 10 times and 20 times high-

er than copper, respectively (Fig. 4).

Therefore, blending copper powder

with diamond, MWCNT, or SWCNT

significantly enhances the thermal

conductivity of thermally managed

components.

It is equally important that the in-

terface between the Cu matrix and sec-

ondary phase (e.g., diamond, MWCNT,

or SWCNT) is adequate for heat transfer.

Electrons dominate heat conduction in

copper, whereas phonons dominate in

second-phase materials including dia-

mond. Therefore, for good heat conduc-

tivity inmetal matrix composites (MMCs),

the energy heat transfer must coordinate

between electrons and phonons.

Other challenges in dealing with

copper and diamond are the large mis-

match in their coefficient of thermal

expansion (CTE) and no chemical bond-

ing, which results in a poor interface and