<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">MSA</journal-id><journal-title-group><journal-title>Materials Sciences and Applications</journal-title></journal-title-group><issn pub-type="epub">2153-117X</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/msa.2017.82013</article-id><article-id pub-id-type="publisher-id">MSA-73992</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Chemistry&amp;Materials Science</subject></subj-group></article-categories><title-group><article-title>
 
 
  Anodic Coating Characteristics of Different Aluminum Alloys for Spacecraft Materials Applications
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Afaf</surname><given-names>M. Abd El-Hameed</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Yehia</surname><given-names>A. Abdel-Aziz</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Fatma</surname><given-names>S. El-Tokhy</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>National Research Institute of Astronomy and Geophysics (NRIAG), Cairo, Egypt</addr-line></aff><aff id="aff2"><addr-line>Faculty of Engineering, El-Zagazig University, Zagazig, Egypt</addr-line></aff><pub-date pub-type="epub"><day>06</day><month>02</month><year>2017</year></pub-date><volume>08</volume><issue>02</issue><fpage>197</fpage><lpage>208</lpage><history><date date-type="received"><day>December</day>	<month>12,</month>	<year>2016</year></date><date date-type="rev-recd"><day>Accepted:</day>	<month>February</month>	<year>5,</year>	</date><date date-type="accepted"><day>February</day>	<month>8,</month>	<year>2017</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
  Anodic oxide coatings on aluminum alloys are used for space environment applications. These provide specific thermo-optical properties to spacecraft surface. Fragments of these coatings lead to generate the contamination in satellites and affect the mission lifetime. The current work concerns studying of the anodic processes applied on aluminum and different groups of aluminum alloys as Al7075, Al2024 and Al6061. Experimental procedures are performed using sulfuric acid at different values of current density (1 - 2 A/dm
  <sup>2</sup>). The influence of the parameters of anodic film formation on the coating characteristics and layer thickness of aluminum alloys has been investigated. Reflectance and optical properties of the anodized aluminum alloy coatings are determined and found to be dependent on the alloying elements. Changes in anodic coating weight and film thickness of aluminium alloys with the process parameters as current density, temperature, time duration, acid concentration, and sealing system have been studied. Moreover, morphology and surface structure of the considered samples are carried out in attempt to understand the physical characteristics. The obtained results are compared and briefly outlined.
 
</p></abstract><kwd-group><kwd>Anodic Oxide Coatings</kwd><kwd> Aluminum Alloy Samples</kwd><kwd> Sulfuric Acid</kwd><kwd> Optical Properties</kwd><kwd> Morphology</kwd><kwd> Analysis</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Aluminum and aluminum alloys have many applications especially in aerospace industries because of their excellent properties such as high strength to weight ratios, low cost, high thermal conductivity and good corrosion resistance. Anodizing is an electrochemical process that is used to form the oxide films on the surface of metals. Anodizing process creates a hard, corrosion- and abrasion-re- sistant oxide coating on aluminum alloys. The anodization layer is formed to adjust and control the thermo-optical properties [<xref ref-type="bibr" rid="scirp.73992-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref2">2</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref3">3</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref4">4</xref>] . Clear anodic oxide coatings have high emissivity and low absorptivity that lead to the efficient radiative heat transfer in the space environment. Aluminum and different groups of aluminum alloys (Al6061, Al2024 and Al7075) are important and widely used, which in particular satisfy the requirements of space applications with good results. As an example, after thermal cycling on aluminum alloys see that in groups 2XXX and 7XXX, some of these alloys have been observed. There- fore, anodizing provides the required optical properties to minimize thermal cycling temperatures and prevent overheating and undercooling in every part of equipment namely good temperature stability of onboard equipments [<xref ref-type="bibr" rid="scirp.73992-ref5">5</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref6">6</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref7">7</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref8">8</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref9">9</xref>] . In the International Space Station (ISS), the micrometeoroid and orbital debris shields are made from anodized aluminum because of its specific thermal properties. The anodizing process is evaluated in regard to throwing power and fatigue life [<xref ref-type="bibr" rid="scirp.73992-ref9">9</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref10">10</xref>] , additionally, anodic coatings can meet not only the environmental requirements but also the continual demand by aerospace and defense hardware for improved surface performance with multifunctional properties to work under extreme environmental exposures (see <xref ref-type="fig" rid="fig1">Figure 1</xref>) [<xref ref-type="bibr" rid="scirp.73992-ref11">11</xref>] . Accordingly, aluminum alloys have a good corrosion resistance for most environmental exposures. Specific environmental conditions may cause corrosion leading to degradation of the surfaces and potentially stress corrosion cracking, causing failure of aluminum alloys. Therefore, anodic coatings have been developed to protect the aluminum from corrosion and enhance the adhesion of paints and adhesives [<xref ref-type="bibr" rid="scirp.73992-ref12">12</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref13">13</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref14">14</xref>] . However, the anodic aluminum coatings mitigate the occurrence of degradation in spacecraft’ surfaces due to space plasma environment effects [<xref ref-type="bibr" rid="scirp.73992-ref15">15</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref16">16</xref>] .</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Multifunctional properties from surface coatings on aluminum alloys for space applications [<xref ref-type="bibr" rid="scirp.73992-ref11">11</xref>] </title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-7701937x2.png"/></fig><p>A wide variety of electrolytes is considered to produce anodic coating on aluminum. According to the solvent action of the electrolyte used for production the anodic film, anodic coatings can be classified. Some of these coatings are of porous and obtained as example from sulfuric electrolyte (Type II). Sulfuric acid is one of the most important anodizing processes because of the characteristics and properties of the film. Different thickness values, clear coating, colored and sealed can be easily obtained. Sulfuric acid anodizing produces coatings with less solar absorptance and high thermal emittance, so, it is common used for thermal control surfaces [<xref ref-type="bibr" rid="scirp.73992-ref17">17</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref18">18</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref19">19</xref>] .</p><p>In the current research, laboratory measurements are carried out to investigate the anodic oxide films produced on aluminum layer and different samples of aluminum alloys. Sulfuric acid anodizing coatings are considered. The anodization parameters as acid concentration, temperature, current density, and sealing process, are taken into account to investigate the physical characteristics and film thickness for the considered samples. Morphology and optical analysis are used to clarify the anodic film behavior. The obtained results of the different samples are compared.</p></sec><sec id="s2"><title>2. Anodic Coatings</title><sec id="s2_1"><title>2.1. Anodic Technique (Oxide Film Formation)</title><p>An electrochemical method (electrolyte solution) is used to anodize the metal surface of aluminum alloys. Because sulfuric acid (Type II) is the most widely used solution to produce anodized coating and provides most corrosion protective finish, the anodic coatings are performed at the laboratory with the concentration of sulfuric acid bath (15 wt% H<sub>2</sub>SO<sub>4</sub>) [<xref ref-type="bibr" rid="scirp.73992-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref20">20</xref>] . In the anodized process, the constant voltage with the value 15 V is applied on the circuit and two operating temperatures (21˚C and 35˚C) are considered in the bath. The thickness coatings formed by this method varies with the anodization parameters. An electric current is introduced into the bath in which the aluminum alloy plate has been immersed. The anodization process is carried out on different types of sample plates seeing that aluminum and different groups of aluminum alloys Al6061, Al2024 and Al7075. These samples are taken with different sizes. The compositions of these alloys are given in <xref ref-type="table" rid="table1">Table 1</xref>. These materials have been used for space applications such that for spacecraft structures, flight hardware, and space devices as onboard and power systems [<xref ref-type="bibr" rid="scirp.73992-ref21">21</xref>] . Moreover, to clarify the impact of electrolyte concentration on the anodic film thickness, 20% by weight</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Aluminum alloys compositions.<sup> </sup></title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Aluminum alloy</th><th align="center" valign="middle" >Compositions*<sup> </sup></th></tr></thead><tr><td align="center" valign="middle" >Al7075</td><td align="center" valign="middle" >5.5% Zn; 2.5% Mg; 1.5% Cu; 0.3% Cr</td></tr><tr><td align="center" valign="middle" >Al2024</td><td align="center" valign="middle" >3.8% to 4.9% Cu; 1.2% to 1.8% Mg; 0.3% to 0.9% Mn; 0% to 0.5% Fe; 0% to 0.5% Si; 0% to 0.25% Zn; 0% to 0.2% Zr; 0% to 0.15% Ti; 0% to 0.1% Cr</td></tr><tr><td align="center" valign="middle" >Al6061</td><td align="center" valign="middle" >0.8% to 1.2% Mg; 0.6% Si; 0.15% Mn; 0.28% Cu; 0.7% Fe</td></tr></tbody></table></table-wrap><p>*Underlines mean the majority of material compositions.</p><p>sulfuric acid is taken in our consideration with the constant voltage 15 V, temperature 21˚C, and current density (2 A/dm<sup>2</sup>). These parameters are applied on the two samples Al6061, and Al2024 for time period 60 minutes of process.</p></sec><sec id="s2_2"><title>2.2. Sealing Process</title><p>Because the coating process is highly porous and is subject to attack from the environment and corrosive elements, sealing process is required to improve surface from cracking and also to improve its resistance to corrosion. The method used to seal the anodic films of the considered samples is the hot water, in which the treated aluminum alloy is immersed in deionized water nearest to the boiling point for 15 minutes. This method may partially convert the alumina of anodic coating to aluminum mono-hydroxide. The mechanism of sealing occurred in boiling water is considered as the hydration of the anodic film. The aluminum oxide reacts with water to form aluminum hydroxide, which fills pores in the coating and seals the surface [<xref ref-type="bibr" rid="scirp.73992-ref22">22</xref>] .</p><disp-formula id="scirp.73992-formula42"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-7701937x3.png"  xlink:type="simple"/></disp-formula><p>From this process, the anodic surface becomes with more flatness and uniformity. This water-sealing technique is used to seal the porous coatings to protect the substrate from attack by environment.</p></sec></sec><sec id="s3"><title>3. Characteristics, Results and Analysis</title><p>The characteristic of anodized coating layer is influenced by the process parameters as current density, temperature, and time duration. One of the most important factors is the current density applied on the samples. This factor is useful to determine the characteristic of the coated layer on aluminium alloy [<xref ref-type="bibr" rid="scirp.73992-ref23">23</xref>] . Two values (1 - 2 A/dm<sup>2</sup>) of the current density are applied in our experiments. Another factor used in this study is the time required for occurrence the coating process. For the oxide film formation, two time intervals 30, 60 minutes are considered for taking place the anodizing process and applied on all sample plates. These values are chosen to examine its effects on the oxide coating thicknesses for different alloy materials. <xref ref-type="table" rid="table2">Table 2</xref> gives the results of the coating thickness for the considered alloys obtained at different parameters of the anodization process. The film thickness d can be calculated for the samples using the formula.</p><disp-formula id="scirp.73992-formula43"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-7701937x4.png"  xlink:type="simple"/></disp-formula><p>where m and m<sub>0</sub> are the weight measured for the anodized sample after and before the anodizing process respectively, obtained from the difference in mass of each sample plate before and after film deposition, A is the area of film on the sample plate, and ρ is the density of the anodic film of aluminium alloys.</p><p>From the results obtained in <xref ref-type="table" rid="table2">Table 2</xref>, it is clearly observed that; at the same time of process:</p><p>1) Increasing current density leads to increase the film thickness;</p><p>2) Lowering bath temperatures result in more dense coating and high thickness values.</p><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> The thickness values of Al-alloys</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Temp. (˚C)</th><th align="center" valign="middle" >Time (min)</th><th align="center" valign="middle" >Alloys</th><th align="center" valign="middle"  colspan="2"  >Coating thickness (μm)</th></tr></thead><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >Current density = 1 A/dm<sup>2 </sup></td><td align="center" valign="middle" >Current density = 2 A/dm<sup>2</sup></td></tr><tr><td align="center" valign="middle"  rowspan="3"  >21</td><td align="center" valign="middle"  rowspan="3"  >30</td><td align="center" valign="middle" >7075</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >3.22</td></tr><tr><td align="center" valign="middle" >2024</td><td align="center" valign="middle" >3.07</td><td align="center" valign="middle" >3.8</td></tr><tr><td align="center" valign="middle" >6061</td><td align="center" valign="middle" >5.85</td><td align="center" valign="middle" >6.55</td></tr><tr><td align="center" valign="middle"  rowspan="3"  >21</td><td align="center" valign="middle"  rowspan="3"  >60</td><td align="center" valign="middle" >7075</td><td align="center" valign="middle" >2.66</td><td align="center" valign="middle" >3.43</td></tr><tr><td align="center" valign="middle" >2024</td><td align="center" valign="middle" >4.07</td><td align="center" valign="middle" >5.24</td></tr><tr><td align="center" valign="middle" >6061</td><td align="center" valign="middle" >10.8</td><td align="center" valign="middle" >13.4</td></tr><tr><td align="center" valign="middle"  rowspan="3"  >35</td><td align="center" valign="middle"  rowspan="3"  >30</td><td align="center" valign="middle" >7075</td><td align="center" valign="middle" >1.8</td><td align="center" valign="middle" >3.12</td></tr><tr><td align="center" valign="middle" >2024</td><td align="center" valign="middle" >2.18</td><td align="center" valign="middle" >2.7</td></tr><tr><td align="center" valign="middle" >6061</td><td align="center" valign="middle" >5.3</td><td align="center" valign="middle" >5.65</td></tr></tbody></table></table-wrap><table-wrap id="table3" ><label><xref ref-type="table" rid="table3">Table 3</xref></label><caption><title> Thickness values of Al-alloys</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Temp. (˚C)</th><th align="center" valign="middle" >Time (min)</th><th align="center" valign="middle" >Current density</th><th align="center" valign="middle"  colspan="2"  >Calculated thickness for Al-alloys (μm)</th></tr></thead><tr><td align="center" valign="middle"  rowspan="2"  >21</td><td align="center" valign="middle"  rowspan="2"  >60</td><td align="center" valign="middle"  rowspan="2"  >2 A/dm<sup>2</sup></td><td align="center" valign="middle" >6061<sup> </sup></td><td align="center" valign="middle" >2024</td></tr><tr><td align="center" valign="middle" >17.1</td><td align="center" valign="middle" >8.3</td></tr></tbody></table></table-wrap><p>The table also clarifies the increase in anodic thickness with time at the same other parameters and conditions of the experiment. These results are valid and correlated with that obtained from many studies [<xref ref-type="bibr" rid="scirp.73992-ref23">23</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref24">24</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref25">25</xref>] [<xref ref-type="bibr" rid="scirp.73992-ref26">26</xref>] .</p><p>To verify the effect of electrolyte concentration on the anodic film thickness, <xref ref-type="table" rid="table3">Table 3</xref> gives the film thickness obtained with 20 wt% sulfuric acid and with the parameters (current density 2 A/dm<sup>2</sup>, temperature 21˚C and time 60 minutes) for the aluminum alloys Al6061 and Al2024 as an example.</p><p>The obtained result shows that, for the for the same two samples considered in <xref ref-type="table" rid="table2">Table 2</xref>, the increasing of the thickness with increase in acid concentration greater than that obtained with 15 wt% acid concentration [<xref ref-type="bibr" rid="scirp.73992-ref27">27</xref>] . It is evident that, anodizing in less acid concentration is performed to obtain a considerably thin anodize layer that gives lower impact on the fatigue strength of the alloy.</p><p>Sealing Effect</p><p>After sealing process (with hot water at 98˚C for 15 minutes) reduction in weight is observed. This is because of the loss in the thickness of anodic oxide film [<xref ref-type="bibr" rid="scirp.73992-ref14">14</xref>] . This loss is due to the dry air (decreasing in humidity, which leads to increasing the weight loss). <xref ref-type="table" rid="table4">Table 4</xref> clarifies the sealing effect of the sample weight for the aluminum alloys after anodization process.</p><p><xref ref-type="table" rid="table5">Table 5</xref> gives an example of the measuring thickness for two samples (Al, and Al6061). The data interpret the decrease in thickness with sealing process for the two considered samples due to the weight loss of the anodic coating films.</p><p>Optical properties</p><p>For the alloy samples, surface structural and properties are considered to investigate the physical characteristics of the anodic films. The optical images of the different anodizing alloys samples are shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>. The images show the coatings are adhered to the substrate. It is interesting to notice that, the sample Al7075 becomes opaque coloring due to the immersion in nickel. The greater opacity of anodic coating Al7075 refers to the dense surface and the alloy elements.</p><p>The optical properties of the anodized aluminum alloy coatings are determined using the instrument “SPECTROMETER/JASCO Corp., V-570, Rev. 1.00”. <xref ref-type="fig" rid="fig3">Figure 3</xref> shows the absorbance spectra of the anodic alloy samples Al6061 (Black) and Al2024 (Red) against the wavelength. The figure characterizes the light absorption of samples in a wide wavelength range from ultraviolet (UV) to infrared (IR) wavelengths (200 nm - 2200 nm). The same behavior is observed for the two considered samples with increasing in values for alloy Al2024. The</p><table-wrap id="table4" ><label><xref ref-type="table" rid="table4">Table 4</xref></label><caption><title> The alloy’s weight without and with sealing process</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Current density</th><th align="center" valign="middle" >Temp. (˚C)</th><th align="center" valign="middle" >Time (min)</th><th align="center" valign="middle" >Alloys</th><th align="center" valign="middle"  colspan="2"  >Weight after anodization</th><th align="center" valign="middle" ></th></tr></thead><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >Without sealing<sup> </sup></td><td align="center" valign="middle" >With sealing</td><td align="center" valign="middle" >The weight loss</td></tr><tr><td align="center" valign="middle"  rowspan="3"  >1 A/dm<sup>2 </sup></td><td align="center" valign="middle"  rowspan="3"  >21</td><td align="center" valign="middle"  rowspan="3"  >30</td><td align="center" valign="middle" >7075</td><td align="center" valign="middle" >20.41</td><td align="center" valign="middle" >20.293</td><td align="center" valign="middle" >0.117</td></tr><tr><td align="center" valign="middle" >2024</td><td align="center" valign="middle" >37.871</td><td align="center" valign="middle" >37.7</td><td align="center" valign="middle" >0.171</td></tr><tr><td align="center" valign="middle" >6061</td><td align="center" valign="middle" >20.3</td><td align="center" valign="middle" >19.592</td><td align="center" valign="middle" >0.708</td></tr><tr><td align="center" valign="middle"  rowspan="3"  >2 A/dm<sup>2</sup></td><td align="center" valign="middle"  rowspan="3"  >21</td><td align="center" valign="middle"  rowspan="3"  >30</td><td align="center" valign="middle" >7075</td><td align="center" valign="middle" >20.1709</td><td align="center" valign="middle" >20.055</td><td align="center" valign="middle" >0.1159</td></tr><tr><td align="center" valign="middle" >2024</td><td align="center" valign="middle" >29.458</td><td align="center" valign="middle" >29.18</td><td align="center" valign="middle" >0.278</td></tr><tr><td align="center" valign="middle" >6061</td><td align="center" valign="middle" >19.963</td><td align="center" valign="middle" >19.619</td><td align="center" valign="middle" >0.344</td></tr></tbody></table></table-wrap><table-wrap id="table5" ><label><xref ref-type="table" rid="table5">Table 5</xref></label><caption><title> Thickness of the samples with and without sealing effect</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Temp. (˚C)</th><th align="center" valign="middle" >Time (min)</th><th align="center" valign="middle" >Metal/alloys</th><th align="center" valign="middle" >Current density</th><th align="center" valign="middle"  colspan="2"  >Measuring thickness (μm)</th></tr></thead><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >A/dm<sup>2</sup></td><td align="center" valign="middle" >Without sealing<sup> </sup></td><td align="center" valign="middle" >With sealing</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >21</td><td align="center" valign="middle"  rowspan="2"  >60</td><td align="center" valign="middle" >Al</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2.6</td><td align="center" valign="middle" >1.5</td></tr><tr><td align="center" valign="middle" >6061</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >13.8</td><td align="center" valign="middle" >12.4</td></tr></tbody></table></table-wrap><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Optical images of anodizing Al-alloy samples</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-7701937x5.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Absorbance of the Al-alloy samples</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-7701937x6.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Reflectance of Al-alloy samples</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-7701937x7.png"/></fig><p>figure exhibits two small peaks at the wavelengths about 800 nm and 2000 nm found in the two samples. In <xref ref-type="fig" rid="fig4">Figure 4</xref>, it is noticed that, from the percent reflectance, the inverse trend is observed. Also the same manner of the two samples is obtained with the decreasing values for alloy Al2024.</p><p>These behaviors are comparable and agreement with that obtained in the experimental work of (Farhat, et al. 2016) [<xref ref-type="bibr" rid="scirp.73992-ref28">28</xref>] . Moreover, spectral absorbance of alloy Al7075 is plotted in <xref ref-type="fig" rid="fig5">Figure 5</xref>. The data are measured for the sample with opaque surface represented in <xref ref-type="fig" rid="fig2">Figure 2</xref>. The figures show different behaviors observed for this sample at the same wavelengths considered in <xref ref-type="fig" rid="fig3">Figure 3</xref> and <xref ref-type="fig" rid="fig4">Figure 4</xref>. Peak values are obtained in the absorbance in visible-region (Vis) about (800 nm) with gradually decreasing in the longer wavelength (IR-region), in which the absorbance becomes with less value. It is seen that, an anodic oxide coating can turn the reflective surface of aluminum into significantly dark, by absorbing most of the impinging visible light. <xref ref-type="fig" rid="fig6">Figure 6</xref> shows the percent reflectance of this sample against the wavelength. Opposite behavior is observed for the reflectance spectra. The figure is similar to the reflectance behavior from black surface coatings. The low-reflectance region extends from 300 nm to 800 nm and more reflectance is obtained for all wavelengths longer than 1000 nm. These results are useful for decreasing unwanted visible radiation in infrared equipment.</p><p>Surface Morphology</p><p>The results of the experiments can be identified by the check of the thickness</p><p>and surface structure of the anodic oxide films on the samples. So, the morphology of the oxide surface for the samples is examined with SEM under the effects of the anodization and sealing processes. <xref ref-type="fig" rid="fig7">Figure 7</xref> shows SEM images of Al6061 anodized surface before (<xref ref-type="fig" rid="fig4">Figure 4</xref>(a)) and after sealing process</p><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Absorbance of alloy Al7075</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-7701937x8.png"/></fig><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Spectral reflectance of alloy Al7075</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-7701937x9.png"/></fig><p>(<xref ref-type="fig" rid="fig4">Figure 4</xref>(b)). Before sealing, some of pores and cracks are observed and distributed on the surface area. After sealing, these pores are relatively diminished and the surface is seen with more flatness and uniformity.</p><p>In <xref ref-type="fig" rid="fig8">Figure 8</xref>, SEM images are taken for the Al-surface for the same conditions considered in <xref ref-type="fig" rid="fig7">Figure 7</xref>. From the figure, it is noticed that, more cracking and incisions are observed (<xref ref-type="fig" rid="fig8">Figure 8</xref>(a)) before sealing, while it is approximated seemed to be vanished after sealing process (<xref ref-type="fig" rid="fig8">Figure 8</xref>(b)). It is logical to expect that anodization of aluminum having impurities leads to defects because of the difference of volume expansion of impurities than of aluminum.</p><fig-group id="fig7"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> SEM images of alloy Al6061 (a) before and (b) after sealing process.</title></caption><fig id ="fig7_1"><label>(b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-7701937x10.png"/></fig><fig id ="fig7_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-7701937x11.png"/></fig></fig-group><fig-group id="fig8"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> SEM images of Al (a) before and (b) after sealing process.</title></caption><fig id ="fig8_1"><label>(b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-7701937x12.png"/></fig><fig id ="fig8_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-7701937x13.png"/></fig></fig-group></sec><sec id="s4"><title>4. Conclusions</title><p>Anodic oxide of aluminum and different types of aluminum alloys as Al2024, Al6061 and Al7075 are prepared by electrochemical method using the solution of sulfuric acid. The effects of different anodizing conditions and parameters are studied. The anodic films are formed on metal surfaces with different thicknesses. To enhance the anodic coating surfaces, we use water-sealing process to seal the porous coatings and find that, the oxide porosity decreases with sealing by pore-filling technique, leading to the oxide layer with more flatness and uniformity. The results show that, the increasing current density and lowering operating temperatures lead to more dense coating. Besides, the increasing of the thickness with increase in acidic concentration is obtained and found greater than that obtained with less acid concentration. The examined optical properties and spectral analysis for the samples demonstrate the dependency on the alloy elements. Morphology and optical characteristics are found to be comparable with the previous studies.</p><p>These results can be useful to obtain optimum anodizing conditions leading to the anodic film formation improving high corrosion resistance and with the best optical characteristics and properties for long-duration exposure to spacecraft external environments.</p></sec><sec id="s5"><title>Cite this paper</title><p>El-Hameed, A.M.A., Abdel-Aziz, Y.A. and El-Tokhy, F.S. (2017) Anodic Coating Characteristics of Different Aluminum Alloys for Spacecraft Materials Applications. Materials Sciences and Applications, 8, 197-208. https://doi.org/10.4236/msa.2017.82013</p></sec></body><back><ref-list><title>References</title><ref id="scirp.73992-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Danford, M.D. (1994) The Corrosion Protection of Several Aluminum Alloys by Chromic Acid and Sulphuric Acid Anodizing. 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