“…51−53 Generally, the adhesion between metal coatings and pristine Kapton substrates approximately range from 7 × 10 −3 to 1.2 × 10 −2 N mm −1 , 54 while our previous work has demonstrated the adhesion between NiCr coating and implanted Kapton is 1.75 ± 0.16 N mm −1 . 3 Therefore, we believe that inorganic Al x Ti y O/ NiCr coating with elevated mechanical stability can be deposited on the Kapton substrate via IIP, FCVA, and HiPIMS.…”
Section: Resultsmentioning
confidence: 99%
“…Phase structures were analyzed using a transmission electron microscope (TEM, TECNAI G20). Adhesive strength and crack resistance were evaluated with a microscratch tester (RST 3 ). The applied constant load was 1 N, and the scratch length was 5.00 mm with a speed of 1.00 mm min −1 .…”
Section: Deposition Of the Almentioning
confidence: 99%
“…During the process of IIP, the interconnection bond networks can be established on the subsurface of the polymer between the implanted species and the polymer unit due to ion stitching and mechanical interlocking effects. 3 The focused ion beam bombardment generated by the magnetic lens in FCVA will promote local epitaxial growth and transformation of the solid solution state. 28 Moreover, the coatings deposited by FCVA always present the characteristics of high compactness, uniformity, and smoothness due to the filtration effect.…”
Section: Introductionmentioning
confidence: 99%
“…Polyimides, such as Kapton HN, are attracting attention for aerospace applications due to their excellent flexibility, lightweight, thermo-optical, and dielectric properties. − Kapton, which is often applied to solar array multilayer isolation systems, thermal control systems, and solar sails, is exposed to the harsh space environment. In the low earth orbit (LEO), external spacecraft materials are subjected to various hazards, such as atomic oxygen (AO), ultraviolet (UV), thermal cycles, debris, and charged particle bombardment. − Currently, various approaches have grown up around the theme of mitigating the AO erosion of Kapton.…”
Polymers
used for the exteriors of spacecraft are always exposed
to risks such as atomic oxygen (AO) or electrostatic discharge (ESD)
degradation. In this work, an Al
x
Ti
y
O/NiCr coating with excellent mechanical stability,
AO durability, and electrostatic dissipative properties was deposited
via ion implantation (IIP), filter cathode vacuum arc (FCVA), and
high-power impulse magnetron sputtering (HiPIMS) on a flexible Kapton
substrate. Scratch and cycle folding tests indicated good adhesion
and toughness of the Al
x
Ti
y
O/NiCr-coated Kapton, which were due to the gradient
structure fabricated by the multitechnology combination. AO exposure
tests demonstrated an extremely low erosion yield (E
y = 5.15 × 10–26 cm3 atom–1) of the Al
x
Ti
y
O/NiCr-coated Kapton, only 1.72% of
that observed for pristine Kapton. Moreover, Rutherford backscattering
spectrometry (RBS) and Kelvin probe force microscopy (KPFM) results
showed that the Al
x
Ti
y
O/NiCr-coated Kapton has elevated surface electrostatic
dissipative properties and sufficient conductivity. The multitechnology
combination offers great flexibility for customizing the gradient
structure to realize a comprehensive performance improvement. In addition,
such a coating has great prospects for aerospace applications.
“…51−53 Generally, the adhesion between metal coatings and pristine Kapton substrates approximately range from 7 × 10 −3 to 1.2 × 10 −2 N mm −1 , 54 while our previous work has demonstrated the adhesion between NiCr coating and implanted Kapton is 1.75 ± 0.16 N mm −1 . 3 Therefore, we believe that inorganic Al x Ti y O/ NiCr coating with elevated mechanical stability can be deposited on the Kapton substrate via IIP, FCVA, and HiPIMS.…”
Section: Resultsmentioning
confidence: 99%
“…Phase structures were analyzed using a transmission electron microscope (TEM, TECNAI G20). Adhesive strength and crack resistance were evaluated with a microscratch tester (RST 3 ). The applied constant load was 1 N, and the scratch length was 5.00 mm with a speed of 1.00 mm min −1 .…”
Section: Deposition Of the Almentioning
confidence: 99%
“…During the process of IIP, the interconnection bond networks can be established on the subsurface of the polymer between the implanted species and the polymer unit due to ion stitching and mechanical interlocking effects. 3 The focused ion beam bombardment generated by the magnetic lens in FCVA will promote local epitaxial growth and transformation of the solid solution state. 28 Moreover, the coatings deposited by FCVA always present the characteristics of high compactness, uniformity, and smoothness due to the filtration effect.…”
Section: Introductionmentioning
confidence: 99%
“…Polyimides, such as Kapton HN, are attracting attention for aerospace applications due to their excellent flexibility, lightweight, thermo-optical, and dielectric properties. − Kapton, which is often applied to solar array multilayer isolation systems, thermal control systems, and solar sails, is exposed to the harsh space environment. In the low earth orbit (LEO), external spacecraft materials are subjected to various hazards, such as atomic oxygen (AO), ultraviolet (UV), thermal cycles, debris, and charged particle bombardment. − Currently, various approaches have grown up around the theme of mitigating the AO erosion of Kapton.…”
Polymers
used for the exteriors of spacecraft are always exposed
to risks such as atomic oxygen (AO) or electrostatic discharge (ESD)
degradation. In this work, an Al
x
Ti
y
O/NiCr coating with excellent mechanical stability,
AO durability, and electrostatic dissipative properties was deposited
via ion implantation (IIP), filter cathode vacuum arc (FCVA), and
high-power impulse magnetron sputtering (HiPIMS) on a flexible Kapton
substrate. Scratch and cycle folding tests indicated good adhesion
and toughness of the Al
x
Ti
y
O/NiCr-coated Kapton, which were due to the gradient
structure fabricated by the multitechnology combination. AO exposure
tests demonstrated an extremely low erosion yield (E
y = 5.15 × 10–26 cm3 atom–1) of the Al
x
Ti
y
O/NiCr-coated Kapton, only 1.72% of
that observed for pristine Kapton. Moreover, Rutherford backscattering
spectrometry (RBS) and Kelvin probe force microscopy (KPFM) results
showed that the Al
x
Ti
y
O/NiCr-coated Kapton has elevated surface electrostatic
dissipative properties and sufficient conductivity. The multitechnology
combination offers great flexibility for customizing the gradient
structure to realize a comprehensive performance improvement. In addition,
such a coating has great prospects for aerospace applications.
“…The good AO erosion-resistance and good adhesion cannot be obtained simultaneously by the inorganic coating. In recent years, in order to solve this problem, gradient coating was proposed, which can improve the bonding performance of coatings by establishing a gradient structure and gradient composition, such as coatings prepared by LAD, plasma polymerization deposition, ion implantation (IIP), filter cathode vacuum arc (FCVA), and electron beam (E-beam) methods [18,23,24]. However, the instruments and procedures for preparing gradient coating are complex and expensive.…”
In this work, the atomic oxygen (AO) erosion-resistance effect and mechanism of the Perhydropolysilazane (PHPS) coating were investigated from the perspective of element distribution in the depth direction. The results revealed that the coating demonstrated good adhesion and intrinsic AO erosion-resistance, which was attributed to the composition gradient formed in the coating. Moreover, the oxygen ratio of the SiOx on top layer of the coating could be elevated during AO exposure, strengthening the Ar ion etching durability of the coating. According to these results, an AO erosion-resistance mechanism model of the PHPS-derived SiOx coating was finally obtained.
Polyimides externally deployed in spacecraft or satellites extensively have various aerospace hazards, including atomic oxygen (AO) erosion, irradiation degradation, and electrostatic charge/discharge (ESC/ESD). To cope with these challenges, we fabricate a ZnO/CuNi‐polyimide composite film with augmented permanence. Using spectroscopy and microscopy techniques, we have shown that the combination of chelation and cross‐linking in the interfacial architecture leads to enhanced interfacial compatibility and mechanical robustness. Besides, due to the positive AO diffusion barrier ability of the wurtzite ZnO, our composite film shows remarkable AO resistance and a very small Ey value of 6.88 × 10−26 cm3/atom, which is merely 2.29% of that of pristine polyimide. Moreover, the well‐defined nanocrystalline state with minimal lattice swelling (0.3%–0.7%) of the Fe+‐irradiated ZnO/CuNi‐polyimide at a damaging dose of 353.4 dpa demonstrates its excellent irradiation resistance. Finally, the ZnO/CuNi‐polyimide also shows sufficient electrostatic dissipation capacity to cope with the ESC/ESD events. Our fabrication approach for composite films based on multi‐technology integration shows potential for aerospace applications and deployment.
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