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<h2 style="text-align:center;">Engine Comparison Table</h2>
<!-- Engine Images -->
<div class="image-container">
<img src="https://upload.wikimedia.org/wikipedia/commons/thumb/d/d3/GE_F404.jpg/500px-GE_F404.jpg" alt="GE F404 IN">
<img src="https://upload.wikimedia.org/wikipedia/commons/thumb/a/a2/GE_F414.jpg/500px-GE_F414.jpg" alt="GE F414">
<img src="https://upload.wikimedia.org/wikipedia/commons/thumb/f/f4/Eurofighter_EJ200.jpg/500px-Eurofighter_EJ200.jpg" alt="EJ2000">
<img src="https://upload.wikimedia.org/wikipedia/commons/thumb/3/3b/Safran_M88.jpg/500px-Safran_M88.jpg" alt="M88">
<img src="https://upload.wikimedia.org/wikipedia/commons/thumb/e/eb/Kaveri_Engine.JPG/500px-Kaveri_Engine.JPG" alt="Kaveri">
<img src="https://upload.wikimedia.org/wikipedia/commons/thumb/5/5b/IHI_XF5_Engine.jpg/500px-IHI_XF5_Engine.jpg" alt="IHI XF5">
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<th>Engine Model</th>
<th>Dimensions (mm)</th>
<th>Bypass Ratio</th>
<th>Compressor Stages</th>
<th>Metallurgy</th>
<th>Thrust Dry (kN)</th>
<th>Thrust Wet (kN)</th>
<th>Overall Pressure Ratio</th>
<th>Engine Type</th>
<th>Source</th>
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<td>GE F404 IN</td>
<td>1,500 x 1,100</td>
<td>0.28</td>
<td>9 (Axial-Flow)</td>
<td>Titanium, Steel</td>
<td>59</td>
<td>83</td>
<td>30</td>
<td>Twin-spool, low-bypass afterburning turbofan</td>
<td>General Electric (GE)</td>
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<tr>
<td>GE F414</td>
<td>1,570 x 1,120</td>
<td>0.32</td>
<td>10 (Axial-Flow)</td>
<td>Titanium, Steel</td>
<td>77</td>
<td>98</td>
<td>32</td>
<td>Twin-spool, low-bypass afterburning turbofan</td>
<td>General Electric (GE)</td>
</tr>
<tr>
<td>EJ 2000</td>
<td>1,530 x 1,200</td>
<td>0.45</td>
<td>12 (Axial-Flow)</td>
<td>Al-Li, Steel</td>
<td>90</td>
<td>100</td>
<td>35</td>
<td>Twin-spool, low-bypass afterburning turbofan (blisks for weight reduction)</td>
<td>Rolls-Royce</td>
</tr>
<tr>
<td>M88</td>
<td>1,600 x 1,200</td>
<td>0.25</td>
<td>10 (Axial-Flow)</td>
<td>Titanium, Steel</td>
<td>75</td>
<td>94</td>
<td>30</td>
<td>Twin-spool, low-bypass afterburning turbofan (FADEC enabled)</td>
<td>Safran</td>
</tr>
<tr>
<td>Kaveri</td>
<td>1,200 x 1,000</td>
<td>0.35</td>
<td>14 (Axial-Flow)</td>
<td>Alloy Steel</td>
<td>50</td>
<td>62</td>
<td>28</td>
<td>Twin-spool, low-bypass afterburning turbofan (Indigenous design)</td>
<td>GTRE</td>
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<tr>
<td>IHI XF5</td>
<td>1,550 x 1,100</td>
<td>0.50</td>
<td>11 (Axial-Flow)</td>
<td>Titanium, Steel</td>
<td>75</td>
<td>95</td>
<td>35</td>
<td>Twin-spool, low-bypass afterburning turbofan (Thrust vectoring enabled)</td>
<td>Mitsubishi Heavy Industries</td>
</tr>
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