DocumentCode :
1889446
Title :
Nano-carbon based vacuum nano-electronic emitters for nano-satellite propulsion
Author :
Nirupama, M.P. ; Bhattacharya, Ashok ; De, Shounak ; Satyanarayana, B.S.
Author_Institution :
R.V.Coll. of Eng., Bangalore, India
fYear :
2015
fDate :
13-17 July 2015
Firstpage :
238
Lastpage :
239
Abstract :
In the age of Internet of Things (IoT), enabled by Information and Communication Technology (ICT), small satellites area expected to play a major role as facilitator. The small satellites has further got a fillip on account of the advancement in the field of science and technology of field assisted electron emission which enables the propulsion of such small satellites. Especially the feasibility of nano carbon based, with high aspect ratio, self aligned structured, chemically stable, low power operating, miniaturization and improved life time, the Field Emission Electrical Propulsion (FEEP) has enhanced the interest in nano and pico satellites. Presented in this study is a brief overview of design, development and establishing of local capability for material and field emission device/array growth, characterization facility for emitters, design and development of arrays, to packaging and development of small satellites in an academic environment.
Keywords :
aerospace propulsion; artificial satellites; carbon nanotubes; electric propulsion; electron field emission; nanoelectronics; nanostructured materials; C; field assisted electron emission; field emission electrical propulsion; nanocarbon based vacuum nanoelectronic emitters; nanosatellite propulsion; Arrays; Carbon dioxide; Current measurement; Plasma temperature; Propulsion; Satellites; Temperature measurement; FEEP; Nano-carbon; Nano-satellite;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Vacuum Nanoelectronics Conference (IVNC), 2015 28th International
Conference_Location :
Guangzhou
Print_ISBN :
978-1-4673-9356-0
Type :
conf
DOI :
10.1109/IVNC.2015.7225595
Filename :
7225595
Link To Document :
بازگشت