NUCLEAR THERMIONIC POWER SYSTEM FOR SPACECRAFT.

被引：0

作者：

Phillips, W.M.

Estabrook, W.C.

Hsieh, T.M.

机构：

来源：

| 1976年 / 2 SAE卷

关键词：

Heat pipes - PROPULSION - Electric Energy - THERMIONIC POWER GENERATION - Nuclear Energy;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Exploration of the outer planets of the solar system requires a nuclear power system with electric propulsion. Thermionic conversion utilizing the out-of-core design will fulfill the requirements of lifetime, redundancy, and safety margin. The effect of various design parameters are presented with a spacecraft configuration meeting the specific weight and size requirements for a single shuttle launch.

引用

页码：1487 / 1493

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