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The Effects of Cure Time and O2 Plasma Exposure
on Epoxy Based Primers for Superhydrophobic
Contamination Control Coating (LOTUS)
Code 546
Mark Hasegawa EngineeringStephen Lebair
The Lotus coating mimics the superhydrophobicity of the Lotus Flower after which it is
named, and can be used to prevent particles from settling on the surface of coating substrates. Lotus
consists of three main compounds. An aluminum substrate, which is surface prepped to remove any
oxides; a binder, which is applied with a small weight percentage of silica nano-particles that vary in size
from 15 nanometers to 80 nanometers; and a self-assembly monolayer (SAM) that creates the low surface
energy of a superhydrophobic system. The SAM is made using 1H,1H,2H,2H-perflorooctyltrichlorosilane.
The fluorinated carbon tail allows for the superhydrophobic traits that are observed. A major problem that
has emerged with Superhydrophobic surface coatings is durability and the Lotus coating is not yet resilient
enough for consistent handling. Production process changes can alter the adhesion characteristics of
Lotus. This caused a change in the cure time of its primer, and/or the addition of oxygen plasma etching.
Therefor, several studies were conducted to investigate the durability effects of shortening cure time, and
O2 plasma exposure.
To be considered “superhydrophobic” the surface contact angle of a water droplet must be
greater than 150 degrees. A surface is considered hydrophobic if the contact angle falls between 130 to 150
degrees. In contrast, a surface contact angle of 90 degrees or less is “hydrophilic” (having an affinity to
water). Surface contact angles are measured with an instrument considered called a goniometer, wherein a
drop of deionized water is placed onto the surface, and its contact angle is measured. Lotus could potentially
provide, a space-stable coating that removes any minute particulate contamination with a quick tip, shake, or
rinse of deionized water. The final goal for Lotus is to be able to apply it to flight hardware, and prevent loss
of superhydrophobic, anti-contamination properties under harsh space environments.
First and foremost, I’d like to thank my mentor, Mark Hasegawa, for supporting this project
and providing the lab equipment to make this research possible. Additionally, I’d like to thank three
colleagues for their groundbreaking contributions to Lotus in the past years: Kenneth O’Connor, Tori
Stotzer, and Alexson Harris-Kirksey. ReferencesGnanappa, A. K., O’Murchu, C., Slattery, O., Peters, F., O’Hara, T., Aszalós-Kiss, B., & Tofail, S. A. M. (2008). Effect of Annealing on Improved
Hydrophobicity of Vapor Phase Deposited Self-Assembled Monolayers. The Journal of Physical Chemistry C, 112(38), 14934–14942. doi:10.1021/jp804745t
Li, J., Xu, J., Fan, L., & Wong, C. P. (2004). Lotus effect coating and its application for microelectromechanical systems stiction prevention. In Electronic
Components and Technology Conference, 2004. Proceedings. 54th (Vol. 1, pp. 943–947). IEEE. Retrieved from http://ieeexplore.ieee.org/xpls/abs_all.jsp?arnumber=1319451
Samuel, B., Zhao, H., & Law, K.-Y. (2011a). Study of Wetting and Adhesion Interactions between Water and Various Polymer and Superhydrophobic
Surfaces. The Journal of Physical Chemistry C, 115(30), 14852–14861. doi:10.1021/jp2032466
Samuel, B., Zhao, H., & Law, K.-Y. (2011b). Study of Wetting and Adhesion Interactions between Water and Various Polymer and Superhydrophobic
Surfaces. The Journal of Physical Chemistry C, 115(30), 14852–14861. doi:10.1021/jp2032466
Yildirim, A., Khudiyev, T., Daglar, B., Budunoglu, H., Okyay, A. K., & Bayindir, M. (2013). Superhydrophobic and Omnidirectional Antireflective Surfaces
from Nanostructured Ormosil Colloids. ACS Applied Materials & Interfaces, 5(3), 853–860. doi:10.1021/am3024417
Zhu, L., Xu, J., Zhang, Z., Hess, D. W., & Wong, C. P. (2005). Lotus effect surface for prevention of microelectromechanical system (MEMS) stiction. In
Electronic Components and Technology Conference, 2005. Proceedings. 55th (pp. 1798–1801). IEEE.
The foundation of epoxies, from a
chemistry standpoint, are epoxide rings which open
to connect with other epoxy molecules. Since
epoxies are polymers, they undergo cross linking
between the individual mers. Heat treatment
(commonly referred to as a “cure”) promotes the
rate at which these mers react.
This research explores the epoxy
layer, and its resistance to physical wear. Our
current formulation can withstand the pressure of a
finger stroke. When ramped up to two pound of
pressure while sliding across the surface, it is
evident that the coating particulates and loses its
superhydrophobicity.Figure 2: SEM image of half-cured MLP-300 w/
silica nano-particles, provided by M. Grossman
Figure 1: Scanning Electron Microscope
(SEM) image of uncured MLP-300 w/ silica
nano-particles, provided by M. Grossman
Figure 9: Cure study of an Huntsman Hybridized
Epoxy, this chart isolates different cure times and
illustrates wear characteristics of the samples
Figure 8: Plasma study of an Huntsman
Hybridized Epoxy, comparisons are made
between O2 plasma exposure and controls on
samples of varying cure lengths
Figure 10: Imaging software
calculates contact angle, volume
S-06242014-2 (Uncured)
Finger Test:
# Left Angle Right Angle Avg Angle Vol (µL)
0 156 156 156 10.219
1 158 158 158 9.335
2 152 153 152.5 12.17
3 156 156 156 7.586
4 154 154 154 8.963
5 154 155 154.5 7.994
6 154 155 154.5 8.632
7 153 154 153.5 8.205
8 153 154 153.5 8.907
Figure 11: Sample spreadsheet of data
used to create finger test graphs
Discussion:
• Cure Study
• The SEM shows that uncured epoxy has a greater surface area than cured epoxy
• Theoretically, an increased surface area should lead to more areas for FOTS to deposit, in
turn creating a lower surface energy
• Experimentally, the cured epoxy was more resistant to physical wear than the half cured
sample, and subsequently the uncured sample
• Unable to conclude why the SEM and the experimental phenomenon regarding initial
contact angle contradict
• Plasma Study
• The epoxies that I’ve tested this summer all have fumed silica and silica nanoparticles
incorporated to increase adhesion to the FOTS and create a nanostructure, respectively
• O2 plasma should etch any surface epoxy down to silica, providing more
adhesion to the FOTS, and a more defined nanostructure, while adding a
penalty to durability
• In every case, regardless of cure time, O2 plasma caused the Lotus coating to degrade in
contact angle retention, while not substantially affecting initial contact angle
• An adhesion study should follow, to see if O2 plasma was beneficial at all
Future Direction with Lotus:
The Lotus coating is currently being further developed for non-space environment applications
including solar panels. We currently are changing our formulation to take advantage of relief from specific
limitations which accrue when working in the space environment. Specifically for solar panels, Lotus will be
focused more on optical clarity and durability, without the hindrance outgassing requirements.
• Contamination Study
• Verify the assumed relationship between contact angle and contamination
• Provide more data on the dust mitigation aspect of Lotus
• Materials Study
• Now that this coating isn’t limited by outgassing requirements, use of more adhesive binder
layers should be explored to increase wear resistance
• The solar panels themselves pose an addition problem: our substrate will change from
aluminum to glass
New Processing Techniques
o Apply FOTS on uncured samples, as well as half-cured samples
o Some samples allowed to cure after FOTS
application
o Run oxygen plasma on uncured, half-cured, and cured samples
o Once FOTS applied, some samples allowed to cure
Figure 5: Thermal vacuum
chamber where plasma is run
Contact Angle Measuring (Sessile Drop Method)
1. A sample is labeled into thirds for finger, 2lb, and 5lb testing
2. The sample is place onto the stage of the goniometer
3. Approximately eight microliters of deionized water is dropped
onto the sample
4. Using the camera in figure 4, a picture is taken of the water
droplet resting on the surface of the sample
5. Using imaging software, one can determine the contact angle
of the droplet as well it’s volume
Wear Testing Method
o An initial “zero wear” contact angle measurement is taken
o The droplet is removed by a techwipe without contaminating the
coating
o The coating is then wore down by one of three set forces
o Finger (Figure 6), Two Pound (Figure 7), Five Pound
o Contact angle is measured after each pass, eight times in total, to
determine hydrophobic degradation
Figure 6: Finger testing for
wear properties
Figure 7: Two pound weight
testing for wear characteristics
Figure 4: Goniometer
Θ
Figure 3: Chemical
structure of a simple epoxy
Methods
Background
Abstract Results
Conclusions
References and Acknowledgements
Science, Discovery, and the Universe