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<div class="container"> | |
<h1>SpaceX Mars Rocket Engine Simulation</h1> | |
<div class="video-container"> | |
<iframe width="420" height="315" src="https://www.youtube.com/embed/vYA0f6R5KAI" frameborder="0" allowfullscreen></iframe> | |
</div> | |
<div class="info-section"> | |
<h2>Raptor Engine Specifications</h2> | |
<div class="stat"> | |
<span class="stat-label">Thrust (sea level):</span> | |
<span>2,200 kN (500,000 lbf)</span> | |
</div> | |
<div class="stat"> | |
<span class="stat-label">Thrust (vacuum):</span> | |
<span>2,600 kN (580,000 lbf)</span> | |
</div> | |
<div class="stat"> | |
<span class="stat-label">Specific impulse (sea level):</span> | |
<span>330 s</span> | |
</div> | |
<div class="stat"> | |
<span class="stat-label">Specific impulse (vacuum):</span> | |
<span>380 s</span> | |
</div> | |
<div class="stat"> | |
<span class="stat-label">Chamber pressure:</span> | |
<span>300 bar (4,350 psi)</span> | |
</div> | |
</div> | |
<div class="info-section"> | |
<h2>Simulation Features</h2> | |
<ul> | |
<li>Real-time combustion dynamics</li> | |
<li>Propellant flow visualization</li> | |
<li>Thermal analysis of engine components</li> | |
<li>Nozzle expansion ratio optimization</li> | |
<li>Turbopump performance metrics</li> | |
</ul> | |
</div> | |
<a href="https://websim.ai/c/spacex-mars-mission" class="cta-button">Explore Full Mars Mission Sim</a> | |
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