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<p>730.</p>

<p>This short wingspan produced little lift at low speed, resulting in long take-off runs and high landing speeds. In an SST design, this would have required enormous engine power to lift off from existing runways, and to provide the fuel needed, "some horribly large aeroplanes" resulted. Based on this, the group considered the concept of an SST infeasible, and instead suggested continued low-level studies into supersonic aerodynamics.</p>

<p><big>Slender deltas</big></p>
<p>Soon after, <a href="page.php?w=Johanna_Weber">Johanna Weber</a> and</p><p>
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