DocumentCode :
2490553
Title :
Design and analyse space radiation shielding for a Nanosatellite in low earth orbit (LEO)
Author :
Mayanbari, Masood ; Kasesaz, Yaser
Author_Institution :
Iran Space Res. Inst., Tehran, Iran
fYear :
2011
fDate :
9-11 June 2011
Firstpage :
489
Lastpage :
493
Abstract :
In this paper we design and analyze space radiation shielding for Nanosatellite with perigee 250 km and apogee 650 km, with endurance one month in solar max activity. At first step space radiation environment simulated. The proton spectrum energy in inner Van Allen belt varies from 0.01 MeV to 400 MeV. In second step radiation shield designed. The shield was made by AL7075. Analyzes done with formula calculation and MCNP-X.
Keywords :
Earth orbit; artificial satellites; shielding; solar radiation; AL7075; LEO; MCNP-X; Van Allen belt; low Earth orbit; nanosatellite; proton spectrum energy; solar max activity; space radiation environment; space radiation shielding; Aluminum; Belts; Low earth orbit satellites; Materials; Orbits; Protons; Analyze proton shielding; Inner Van Allen belt simulation; Nanosatellite radiation shielding; Space proton protection; Space simulation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies (RAST), 2011 5th International Conference on
Conference_Location :
Istanbul
Print_ISBN :
978-1-4244-9617-4
Type :
conf
DOI :
10.1109/RAST.2011.5966883
Filename :
5966883
Link To Document :
بازگشت