A space solar thermophotovoltaic power system

Author

Stone, K.W. ; Drubka, R.E. ; Kusek, S.M.

Author_Institution

McDonnell Douglas Electron. Syst. Co., Huntington Beach, CA

Volume

2

fYear

1996

fDate

11-16 Aug 1996

Firstpage

1001

Abstract

A solar thermophotovoltaic (STPV) power system is a competitive option for future space missions. This paper describes the principle of operation of a STPV system, the conceptual design of the thermophotovoltaic (TPV) conversion unit and some of the operating features which make it attractive for space applications. McDonnell Douglas Aerospace (MDA) has conducted over 550 hours of on-Sun tests using a 90 kW_t solar concentrator and additional smaller scale laboratory tests. During these tests, various materials and components have been tested at temperatures above 1300°C. The results of these tests have been used to verify analytical models of the subsystems. These models were integrated into a simulation to estimate the system performance. A summary of the on-Sun testing, small scale laboratory testing and estimate of system efficiency is presented. The mass and performance characteristics of a 25 kW_e space system are presented

Keywords

aerospace simulation; aerospace testing; design engineering; photovoltaic cells; space vehicle power plants; 25 kW; 550 h; 90 kW; analytical models; conceptual design; laboratory testing; mass characteristics; performance characteristics; space missions; space solar thermophotovoltaic power system; Aerospace materials; Aerospace testing; Analytical models; Conducting materials; Laboratories; Materials testing; Power systems; Space missions; System testing; Temperature;

fLanguage

English

Publisher

ieee

Conference_Titel

Energy Conversion Engineering Conference, 1996. IECEC 96., Proceedings of the 31st Intersociety

Conference_Location

Washington, DC

ISSN

1089-3547

Print_ISBN

0-7803-3547-3

Type

conf

DOI

10.1109/IECEC.1996.553835

Filename

553835