Advanced solar Brayton space power systems

Author

Pietsch, Anthony ; Brandes, Donald J.

Author_Institution

Allied-Signal Aerosp. Co., Tempe, AZ, USA

fYear

1989

fDate

6-11 Aug 1989

Firstpage

911

Abstract

The closed-Brayton-cycle space power system has been selected to supply electric power for the NASA space station and military space applications. These systems are based on well-proven superalloy metal technology that limits the turbine inlet temperature to the range of 1033 to 1144 K (1400 to 1600°F). Significant performance improvements can be attained by increasing the turbine inlet temperature to the range of 1367 to 1644 K (2000 to 2500°F). Development in ceramic and composite materials for gas turbines show promise for increasing the temperature of the closed Brayton cycle system to this range. These technologies and the improvements in solar-powered closed Brayton cycle power system performance that can be gained are discussed

Keywords

gas turbines; heat engines; photovoltaic power systems; space vehicle power plants; 1400 to 1600 degF; 2000 to 2500 degF; NASA space station; ceramic; composite materials; electric power supply; military space applications; solar Brayton space power systems; turbine inlet temperature; Aerospace materials; Aircraft; NASA; Power system reliability; Power systems; Space stations; Space technology; Temperature distribution; Testing; Turbines;

fLanguage

English

Publisher

ieee

Conference_Titel

Energy Conversion Engineering Conference, 1989. IECEC-89., Proceedings of the 24th Intersociety

Conference_Location

Washington, DC

Type

conf

DOI

10.1109/IECEC.1989.74577

Filename

74577