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Comments on 'First Interstellar Missions, Considering Energy And Incessant Obsolescence'

机译:评论“第一次星际任务,考虑到能量和持续的过时”

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I note with interest the recent paper [1] by Millis. In particular I wish to highlight the discussion on the first launch of a Colony Ship being at least 200 years away due to the total energy expenditure in comparison to an average space shuttle launch. The analysis needs reworking due to an incorrect assumption. The author assumed a velocity increment of just 42 km/s using a rocket with an exhaust velocity of 9,000 km/s. This is far from optimal for the assumed velocity increment. Rockets achieve a maximum energy efficiency when the exhaust velocity is approximately 5/8 of the velocity increment i.e. a mass ratio of 4.92. Hermann Noordung [2] derived this as long ago as 1929, while Les Shepherd's seminal article, "Interstellar Flight" [3] published in this journal, also makes use of this theorem. Thus the actual velocity increment for the 4.8E18 J scenario assumed by the author of reference [1] is 500 km/s for a 25,000 tonne Colony Ship.
机译:我感兴趣地注意到Millis的最新论文[1]。我尤其要特别强调关于首次发射至少200年以来的殖民飞船的讨论,这是因为与平均航天飞机发射相比,其总能量消耗大。由于不正确的假设,因此需要重新进行分析。作者假设使用排气速度为9,000 km / s的火箭,速度仅增加42 km / s。对于假定的速度增量,这远非最佳。当排气速度约为速度增量的5/8(即质量比为4.92)时,火箭将获得最大的能量效率。早在1929年,Hermann Noordung [2]就得出了这一定理,而在该期刊上发表的Les Shepherd的开创性文章“星际飞行” [3]也利用了该定理。因此,对于25,000吨的殖民船,参考文献[1]的作者假设的4.8E18 J情景的实际速度增量为500 km / s。

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