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From this web page, the weight of the shuttle external tank with the
liquid oxygen and hydrogen is 1.6 million pounds: EXTERNAL TANK http://science.ksc.nasa.gov/shuttle/...ewsref/et.html But the amount of liquid oxygen that is burned is only 2,787 pounds per second and the amount of hydrogen 465 pounds per second. Nanotube productions methods are advancing quickly. Suppose it is possible to make a fuel line of carbon nanotube material hundreds of kilometers long. Could fuel be pumped up to a rocket accelerating to orbital velocity? What would be the fuel requirements for a rocket that did not carry its own fuel? Say a rocket with the payload capacity of the shuttle and with engines of the efficiency of the shuttle main engines? Bob Clark |
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