DocumentCode
304192
Title
Reliable compact electrical power source systems for space launch vehicles
Author
Young, Allen R.
Author_Institution
Allied Signal Equipment Syst., Torrance, CA, USA
Volume
1
fYear
1996
fDate
11-16 Aug 1996
Firstpage
650
Abstract
The author describes several key technologies utilized in the design of a family of direct-drive turboalternator systems for space launch vehicles. These systems automatically provide conditioned and regulated electrical power at various voltages, powering actuators, valves and avionics throughout the vehicle. The simple and robust ring-wound two-pole toothless alternator operates at peripheral speeds, making it suitable to be driven directly by a turbine, thereby eliminating the weight, reliability, zero “g” lubrication and cooling issues of a speed-reducing gearbox, while allowing the turbine to operate at reasonable efficiency. Additionally, the use of self-aligning foil bearing and catalytic combustors or cold gas propellants enhance the reliability. The power conditioner and electronic controller provide “hands-off” regulated AC or DC power on demand, maintaining critical parameters within established limits and performance while reporting on built-in health-monitoring tests
Keywords
alternators; machine bearings; reliability; space vehicle power plants; turbogenerators; catalytic combustors; cold gas propellants; compact electrical power source; direct-drive turboalternator; key technologies; performance; reliability enhancement; ring-wound two-pole toothless alternator; self-aligning foil bearing; space launch vehicles; Actuators; Aerospace electronics; Alternators; Power system reliability; Robustness; Space technology; Space vehicles; Turbines; Valves; Voltage;
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.1996.552970
Filename
552970
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