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

页码：139 / 152

页数：14

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