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- W2023707272 abstract "Recent investigations have indicated that it may be possible to generate and store antiprotons in quantities sufficient to propel rockets to the nearer stars. Annihilating these antiprotons with matter would yield energy in the form of relativistic particles. These particles could then be used to heat a propellent and provide thrust. Building a rocket capable of propelling vehicles to the stars is well beyond the current technology. Nevertheless, it is possible to devise annihilation rockets with considerably less performance, requiring only minor extrapolations of current technology. As an orbital transfer vehicle such a rocket could use a standard DeLaval nozzle with a 100:1 area ratio. The combustion chamber would be 2 m in diameter, operating at 100 atm and a temperature slightly above the boiling point of water. The relativistic particles, created during the annihilation, would be trapped in a 50-500 kG magnetic field and would be used to heat liquid hydrogen. The high-magnetic fields required for confinement appear to be the major design concern. Once such a rocket is built it becomes a matter of engineering improvements to realize the ultimate potential performance of mass annihilation rockets." @default.
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- W2023707272 date "1985-03-01" @default.
- W2023707272 modified "2023-09-25" @default.
- W2023707272 title "Antimatter propulsion for OTV applications" @default.
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