DocumentCode
3219397
Title
Space power technology
Author
Rose, M. Frank
Author_Institution
Space Power Inst., Auburn Univ., AL, USA
fYear
1996
fDate
25-27 Jun 1996
Firstpage
9
Lastpage
14
Abstract
The trends today are toward smaller satellites with increased capability. These two trends place enormous demands on the technology used to power such space systems. Typical power sources are nuclear, photovoltaic, and chemical. As the power available on a typical satellite decreases, the use of long pulsed power sources becomes more attractive. Technologies such as electrochemical capacitors, pulsed batteries and flywheels offer the possibility of employing high power subsystems for limited times without undue burden on the spacecraft power train. The state of the art in each of the pulsed storage devices is discussed and preliminary experiments described which use an electrochemical power source to power a spacecraft propulsion unit such as an arc-jet or Hall effect thruster
Keywords
aerospace engines; aerospace propulsion; energy storage; pulsed power technology; space vehicle power plants; Hall effect thruster; arc-jet; electrochemical capacitors; flywheels; pulsed batteries; pulsed power sources; pulsed storage devices; satellites; space power technology; spacecraft power train; spacecraft propulsion unit; state of the art; Batteries; Capacitors; Chemical technology; Flywheels; Photovoltaic systems; Propulsion; Satellites; Solar power generation; Space technology; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Modulator Symposium, 1996., Twenty-Second International
Conference_Location
Boca Raton, FL
Print_ISBN
0-7803-3076-5
Type
conf
DOI
10.1109/MODSYM.1996.564436
Filename
564436
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