Hollow polyimide shells, for use as ICF targets, were fabricated by co-depo
siting monomer precursors from the vapor phase onto bounced spherical mandr
els. The process involved two stages: first, the deposited monomers (pyrome
llitic dianhydride and 4,4'-oxydianiline) reacted on the mandrel surface to
form polyamic acid; second, the mandrel was heated to 300 degrees C to imi
dize the polyamic acid and to decompose the mandrel. During this latter pro
cess the decomposed mandrel diffused through the thermally stable coating,
leaving a polyimide shell. Depositions were performed under low (similar to
10(-3) Torr) and high (similar to 10(-6) Torr) vacuum. Also, flat witness
films of polyimide deposited on Si wafers and NaCl allowed the mechanical p
roperties and chemical composition of the film during the heating cycle to
be measured. Polyimide shells with diameters ranging from 700 to 950 mu m a
nd wall thicknesses ranging from 2 to 13 mu m were produced. The shell's sp
hericity was greater than 99%. Burst and buckle pressure tests on these she
lls yielded the estimated mechanical strength properties. The elastic modul
us and tensile strength were similar to 15 GPa and similar to 300 MPa, resp
ectively. The permeability of D-2 through polyamic acid at 25 degrees C was
7.4 x 10(-17) mol.m/m(2).Pa.s and increased to 6.4 x 10(-16) mol.m/m(2).Pa
.s at 25 degrees C upon curing the shell to 150 degrees C. The permeability
of D-2 at 25 degrees C through vapor-deposited polyimide flat films was me
asured to be 240 times greater than through the as-deposited polyamic acid,
and about 7 times greater than through commerially available solution-cast
Kapton.