Two-stage concentrators for solar bimodal power and propulsion systems

被引：0

作者：

Ender, AY ^{[1
]}

Kolyshkin, IN ^{[1
]}

Kuznetsov, VI ^{[1
]}

机构：

[1] AF Ioffe Phys Tech Inst, St Petersburg 194021, Russia

来源：

IECEC-97 - PROCEEDINGS OF THE THIRTY-SECOND INTERSOCIETY ENERGY CONVERSION ENGINEERING CONFERENCE, VOLS 1-4: VOL.1: AEROSPACE POWER SYSTEMS AND TECHNOL; VOL 2: ELECTROCHEMICAL TECHNOL, CONVERSION TECHNOL, THERMAL MANAGEMENT; VOLS 3: ENERGY SYSTEMS, RENEWABLE ENERGY RESOURCES, ENVIRONMENTAL IMPACT, POLICY IMPACTS ON ENERGY; VOL 4: POST DEADLINE PAPERS, INDEX | 1997年

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A solar bimodal system provides both electrical power for an on-orbit operation and high-performance thermal propulsion capability for an orbital transfer. An orbital transfer payload strongly depends on solar concentrator mass which is determined by its efficiency. This paper is devoted to analysis and comparison of concentrator-receiver system efficiency for one- and two-stage solar concentrators. A new computer code TANDEM for calculating the concentrator-receiver system efficiency was developed. The basic principles of this code are discussed.

引用

页码：422 / 426

页数：5

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