Bimodal solar thermionic power and propulsion system

被引:0
作者
N. N. Ponomarev-Stepnoi
V. A. Usov
A. S. Koroteev
V. N. Akimov
N. I. Arkhangel’skii
Yu. V. Nikolaev
A. S. Gontar’
R. N. Maraginskii
E. N. Sokolov
A. V. Klimov
E. D. Avdoshin
机构
[1] Russian Science Center Kurchatov Institute,
[2] M. V. Keldysh Research Center,undefined
[3] Scientific Research Institute of the Scientific and Industrial Association Luch,undefined
[4] Central Design Office of Machine Building,undefined
[5] Close Joint-Stock Company NP Énergotekh,undefined
来源
Atomic Energy | 2000年 / 89卷
关键词
Geostationary Orbit; Thermionic Converter; Solar Concentrator; Cesium Vapor; Target Orbit;
D O I
暂无
中图分类号
学科分类号
摘要
A conceptual design of a solar power and propulsion thermionic system tied to a Rus’ carrier rocket was developed in the period 1997–1999. In the course of this work, all basic components were analyzed, a cost estimate was made, the scheme for placing the system in orbit, the operating regimes, special features of the adopted concept, as well as the mass, were determined, and the appearance of a system with a useful electrical power of at least 6 kW was formulated.
引用
收藏
页码:516 / 519
页数:3
相关论文
empty
未找到相关数据