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<p>Aviation's Aerophysics Laboratory published a large paper surveying many of the problems involved in using nuclear reactors to power airplanes and rockets. The study was specifically aimed at an aircraft with a range of 10000 mi and a payload of 8000 lb, and covered <a href="page.php?w=turbopump">turbopump</a>s, structure, tankage, <a href="page.php?w=aerodynamics">aerodynamics</a> and <a href="page.php?w=nuclear_reactor">nuclear reactor</a> design. They concluded that hydrogen was best as a propellant and that <a href="page.php?w=graphite">graphite</a></p><p>
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