Nuclear Salt Water Rocket
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The nuclear salt water rocket possibly the craziest rocket engine ever imagined.
Nuclear salt water rocket. For one thing this beast is so wildly dangerous we would have to assemble the craft itself in orbit high orbit maybe at a lagrange. 1 in place of traditional chemical propellant such as that in a chemical rocket the rocket would be fueled by salts of plutonium or 20 percent enriched uranium. Evil chuckle oooh yes indeed.
Ns wr is constructed. The basis of a novel space propulsion system called a nuclear salt water rocket nswr is outlined. Of a bundle of boron carbide coated pipes each containing an aqueous solution of uranium or plutonium salt these pipes.
Nuclear salt water rocket a nuclear salt water rocket or nswr is a proposed type of nuclear thermal rocket designed by robert zubrin that would be fueled by water bearing dissolved salts of plutonium or u 235. So if you want to get to titan in 263 days the nuclear salt water rocket is your vehicle. The nuclear salt water rocket is a rocket engine concept that uses a rapid nuclear reaction in a uranium salt dissolved in water to create a high thrust high efficiency engine which eclipses the performance of any rocket engine ever designed.
Empty into a single long cylindrical plenum pipe of larger diameter which terminates in a rocket nozzle. A nuclear salt water rocket should be able to reach 66 km per second since titan is 10 au away that is 1 500 000 000 kilometers divide that by 66 km sec and we get 22 700 000 seconds which equals 263 days. In place of traditional chemical propellant such as that in a chemical rocket the rocket would be fueled by salts of plutonium or 20 percent enriched uranium the solution would be contained in a bundle of pipes coated in boron carbide for its properties of neutron absorption.
The nuclear salt water rocket possibly the craziest rocket engine ever imagined. But this is serious mad science here and we need to go about it appropriately. The great thing about single h is that in a solid core nuclear thermal rocket it has double the exhaust velocity and specific impulse of ordinary h 2 molecular hydrogen.
This is because the exhaust velocity increases as the mass of the propellant particle decreases.
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