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首页> 外文期刊>Journal of the British Interplanetary Scoiety >ANTIMATTER ASSISTED INERTIAL CONFINEMENT FUSION PROPULSION SYSTEMS FOR INTERSTELLAR MISSIONS
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ANTIMATTER ASSISTED INERTIAL CONFINEMENT FUSION PROPULSION SYSTEMS FOR INTERSTELLAR MISSIONS

机译:星际任务的反辅助惯性约束融合推进系统

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摘要

Current developments such as the Ion Compressed Antimatter Nuclear (ICAN-II) propulsion system proposed by the Pennsylvania State University Center for Space Propulsion Engineering open way to the possible use of available supplies of antiprotons to power antimatter assisted inertial confinement fusion(AAICF) propulsion systems for interstellar missions. Analysis indicates that light weight AAICF propulsion systems with specific impulses in excess of seven hundred thousand seconds may be feasible within the next 30 years. AAICF should prove to be the optimum propulsion system since it possesses high thrust, low weight and high exhaust velocity. The purpose of this paper is to evaluate the potential of AAICF propulsion for interstellar missions such as NASA Administrator Dan Golding's Alpha Centauri Flyby and a Barnard's Star Orbital Mission, and to compare these projections with previous performance estimates for ICF Laser Beam propulsion systems.
机译:宾夕法尼亚州立大学空间推进工程中心提出的诸如离子压缩反物质核(ICAN-II)推进系统的最新发展为可能使用反质子提供动力为反物质辅助惯性约束聚变(AAICF)推进系统开辟了道路用于星际任务。分析表明,在未来30年内,具有超过70万秒的特定脉冲的轻型AAICF推进系统可能是可行的。 AAICF应该被证明是最佳的推进系统,因为它具有高推力,低重量和高排气速度。本文的目的是评估AAICF推进在诸如NASA局长丹·戈尔丁(Dan Golding)的Alpha Centauri Flyby和巴纳德(Barnard)的星轨道任务等星际任务中的潜力,并将这些预测与以前对ICF激光束推进系统的性能估算进行比较。

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