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<p>called for a vehicle capable of putting 20000 to 40000 lb into orbit, or accelerating 6000 to 11900 kg to <a href="page.php?w=trans-lunar_injection">trans-lunar injection</a>. Existing U.S. launchers could place a maximum of about 3900 lb in orbit, but might be expanded to as much as 9900 lb with new high-energy upper stages. In any event, these upper stages would not be available until 1961 at the earliest, and would still not meet the DoD requirements for heavy loads.</p>

<p><a href="page.php?w=Wernher_von_Braun">Wernher von Braun</a>'s team</p><p>
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