离心式核热力火箭燃料元件多孔圆柱形容器的数值研究

IF 1.5 4区工程技术 Q2 NUCLEAR SCIENCE & TECHNOLOGY

Nuclear Technology Pub Date : 2024-07-02 DOI:10.1080/00295450.2024.2361185

Pramatha Bhat, Kendall R. Adams, Stephen J. Herring, Brad Kirkwood

引用次数: 0

摘要

在深空推进和星际探索方面，离心核热火箭（CNTR）有能力达到非常高的比冲（Isp）指标，超过常规火箭。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

Numerical Study of Porous Cylindrical Containment for the Fuel Element of a Centrifugal Nuclear Thermal Rocket

For deep-space propulsion and interplanetary exploration, the centrifugal nuclear thermal rocket (CNTR) has the ability to achieve a very high specific impulse (Isp) metric beyond that of conventio...

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

Nuclear Technology 工程技术-核科学技术

CiteScore

3.40

自引率

6.70%

发文量

116

审稿时长

4-8 weeks

期刊介绍： Nuclear Technology aims to be the leading international publication reporting new information in the practical applications of nuclear science and technology. We publish technical papers, technical notes, critical reviews, rapid communications, book reviews, and letters to the editor on all phases of applications of fundamental research to nuclear technology.