THEORETICAL STUDY OF A NUCLEAR JET ENGINE FOR THE PROPULSION OF AIRPLANES

被引：0
|
作者：
Mitrica, Bogdan [1 ]
Stanciu, Virgil
Petre, Marian [1 ]
Dima, Mihai [1 ]
Badita, Chivuta [1 ]
Precup, Irinel [1 ]
Petre, Carmelia [1 ]
机构：
[1] Univ POLITEHN Bucuresti, Fac Ingn Aerospatiala, Bucharest, Romania
来源：
UNIVERSITY POLITEHNICA OF BUCHAREST SCIENTIFIC BULLETIN-SERIES A-APPLIED MATHEMATICS AND PHYSICS | 2011年 / 73卷 / 04期
关键词：
nuclear reactor; jet engine; propulsion; airplane;
D O I：
暂无
中图分类号：
O29 [应用数学];
学科分类号：
070104 ;
摘要：
Investigation of the possibility to use a nuclear reactor for the propulsion of airplanes could be performed considering two possible solutions: the direct cycle (the fluid pass through the reactors core) and the indirect cycle (the fluid pass through a heat exchanger). We report about a complete theoretical study which has been performed for the indirect cycles. The cycles, the characteristics and the performances of nuclear jet engine have been calculated. For the nuclear reactor, a homogenous type using UO(2) as fuel, BeO as neutron moderator and B(4)C as the material for the control rods, has been considerate.
引用
收藏
页码：139 / 152
页数：14
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