文章基本信息

标题：Optimum Staging with Varying Thrust Attitude Angle
本地全文：下载
作者：T. N. Srivastava
期刊名称：Defence Science Journal
印刷版ISSN：0976-464X
出版年度：2014
卷号：16
期号：3
页码：153-164
DOI：10.14429/dsj.16.7243
语种：English
出版社：Defence Scientific Information & Documentation Centre
摘要：Optimum staging programme for step rockets of arbitrary number of stages having different specific impulses and mass fractions with stages is derived, the optimization criterion being minimum take-off weight for a desired burntout velocity at an assigned altitude. Variation of thrust attitude angle from stage to stage and effects of gravity factor are taken into account. Analysis is performed for a degenerate problem obtained by relaxing the altitude constraint and it has been shown that problems of Weisbord, Subotowicz, Hall & Zambelli and Malina & Summerfield are the particular cases of the degenerate problem.
关键词：Optimum staging programme;Mass fractions;Arbitrary number