Kk. Degroh et Ba. Banks, ATOMIC-OXYGEN UNDERCUTTING OF LONG-DURATION EXPOSURE FACILITY ALUMINIZED-KAPTON MULTILAYER INSULATION, Journal of spacecraft and rockets, 31(4), 1994, pp. 656-664
Atomic-oxygen undercutting is a potential threat to vulnerable spacecr
aft materials which have atomic-oxygen protective coatings. Such under
cutting is due to the atomic-oxygen attack of oxidizable materials at
microscopic defects in the protective coatings. These defects occur du
ring fabrication and handling, or from micrometeroid and debris bombar
dment in space. An aluminized-polyimide Kapton multilayer insulation s
ample that was located on the leading edge of the Long Duration Exposu
re Facility has been used to study low Earth orbit atomic-oxygen under
cutting. Cracks in the aluminized coating located around vent holes pr
ovided excellent defect sites for the evaluation of atomic-oxygen unde
rcutting. The experimentally observed undercut profiles were compared
to predictions from Monte Carlo models for normal incident space ram a
tomic-oxygen attack. The shape of the undercut profile was found to va
ry with crack width, which is proportional to the number of oxygen ato
ms entering the crack. The resulting profiles of atomic-oxygen undercu
tting which occurred on the aluminized-Kapton sample indicated wide un
dercut cavities in spite of the fixed ram orientation. Potential cause
s of the observed undercutting are presented. Implications of the unde
rcutting profiles relevant to Space Station Freedom are also discussed
.