A generalization of the rocket formula and its application to advanced space propulsion systems

L.Nasi; J.-L.Raimbault

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A generalization of the rocket formula and its application to advanced space propulsion systems

机译：火箭公式的推广及其在先进空间推进系统中的应用

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摘要

A generalized rocket formula is derived from a first principles approach. The resulting expression of the thrust is applied to advanced space propulsion systems and a possible link between the asymptotic propellant velocity and the velocity at thruster exit is given. An estimation of the thrust modification due to spacecraft-plume interactions is also considered.

机译：通用的火箭公式是从第一原理方法得出的。推力的最终表达式被应用于先进的空间推进系统，并给出了渐近推进剂速度与推进器出口速度之间的可能联系。还考虑了由于航天器-浮子相互作用而引起的推力变化的估计。

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来源
《Acta astronautica》 |2011年第2期|p.34-38|共5页
作者
L.Nasi; J.-L.Raimbault;
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作者单位

Laboratoire de Physique des Plasmas, Ecole Polytechnique, Universite Paris-Sud 11, UPMC, CNRS, 91128 Palaiseau cedex, France;

rnLaboratoire de Physique des Plasmas, Ecole Polytechnique, Universite Paris-Sud 11, UPMC, CNRS, 91128 Palaiseau cedex, France;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词
rocket formula; advanced propulsion; spacecraft-plume interactions;

机译：火箭公式推进力航天器-流体相互作用;

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A generalization of the rocket formula and its application to advanced space propulsion systems

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