DocumentCode :
1121786
Title :
Empirical Solar Proton Model for Orbiting Spacecraft Applications
Author :
Stassinopoulos, E.G. ; King, J.H.
Author_Institution :
NASA-Goddard Space Flight Center Greenbelt, Md. 20771
Issue :
4
fYear :
1974
fDate :
7/1/1974 12:00:00 AM
Firstpage :
442
Lastpage :
450
Abstract :
An empirical model for energetic solar proton fluxes is presented. With this model the effects of such protons on geocentric space missions, to be flown during the next solar active period (1977-1983), and with orbits involving partial magnetospheric shielding, may be estimated. A synoptic background review is given, followed by a detailed discussion of the model´s use, errors, uncertainties, and limitations, including sample calculations which demonstrate the application of specific or general project missions. Finally, for circular trajectories, percentage exposure maps are presented, depicting fractional mission times spent outside particular L shells as functions of orbit altitude and inclination. The distinguishing assumptions of this analysis are: 1) that the solar proton flux in the 10-100 MeV energy range, as accumulated over solar cycle 20 due to several discrete events, will be accumulated at a uniform rate for the seven active years of solar cycle 21; and 2) that all protons in the energy range of interest have a common geomagnetic latitude cutoff.
Keywords :
Magnetic flux; Magnetic shielding; Magnetosphere; Orbital calculations; Orbits; Protons; Space missions; Space vehicles; Trajectory; Uncertainty;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1974.307797
Filename :
4101249
Link To Document :
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