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
Link To Document :
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