DocumentCode :
135589
Title :
Spacecraft electrical power systems (EPS) using the Flyback converters
Author :
Halder, T.
Author_Institution :
Kalyani Gov. Eng. Coll., Kalyani, India
fYear :
2014
fDate :
16-17 Jan. 2014
Firstpage :
52
Lastpage :
57
Abstract :
The paper depicts generation of solar power by the charge controller skills to charge the battery bank at a persnickety voltage during the sunbeams by the Flyback converter to make use of this power at spacecraft power systems during the orbital night or when the load demand goes beyond the solar booth or array capacity. All bits and pieces are supervised by the Flyback power supply entity as light weight, high power density, solid size, least cost, stumpy silhouette, low volume, tight regulations, fine design, high reliability, least failure rate and high efficiency as EPS of a spacecraft.
Keywords :
aircraft power systems; power convertors; solar powered vehicles; EPS; battery bank; charge controller skills; flyback converters; high power density; least failure rate; load demand; solar array capacity; solar booth capacity; spacecraft electrical power system; stumpy silhouette; sunbeams; Capacitors; Engines; Generators; Indexes; MOSFET; Resistors; Switches; Designs; Reliability and Results; Solar power; Spacecraft power supply systems; failure rate; thermal limits;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Non Conventional Energy (ICONCE), 2014 1st International Conference on
Conference_Location :
Kalyani
Print_ISBN :
978-1-4799-3339-6
Type :
conf
DOI :
10.1109/ICONCE.2014.6808681
Filename :
6808681
Link To Document :
بازگشت