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<p>The dragon's first stage was a <a href="page.php?w=Stromboli_engine">Stromboli engine</a> (diameter 56&nbsp;cm) which burned 675&nbsp;kg of propellant in 16 seconds and so produced a maximum thrust of 88&nbsp;kN. Versions of the <a href="page.php?w=B%C3%A9lier_%28rocket%29">Bélier</a> engine were used as upper stages. </p>

<p>A payload of 30 to 120&nbsp;kg could be carried on parabolic with apogees between 440&nbsp;km (270&nbsp;mi) (Dragon-2B) and 560&nbsp;km (340&nbsp;mi)(Dragon-3)</p>

<p><big> Versions </big></p>
<p>The Dragon was built in several</p><p>
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