Title :
Spacecraft electrical power systems (EPS) using the Flyback converters
Author_Institution :
Kalyani Gov. Eng. Coll., Kalyani, India
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;
Conference_Titel :
Non Conventional Energy (ICONCE), 2014 1st International Conference on
Conference_Location :
Kalyani
Print_ISBN :
978-1-4799-3339-6
DOI :
10.1109/ICONCE.2014.6808681