Calculating low-altitude trapped particle fluxes with the NASA models AP-8 and AE-8
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Discipline
Physical sciences
Subject
Calculations
Computer software
Magnetic field effects
Mathematical models
Protons
Radiation belts
Radiation analysis
Trapped particle fluxes
Trapped radiation models
Radiation
proton
article
astronomy
Atlantic Ocean
computer program
electron
Flight Experiment
LDEF Project
long duration
magnetism
radiation dose
radiation monitoring
solar energy
South America
space flight
statistics
theoretical model
unmanned
Flight Experiment
LDEF Project
long duration
unmanned
Atlantic Ocean
Earth (Planet)
Electrons
Magnetics
Models, Theoretical
Protons
Radiation Dosage
Radiation Monitoring
Software
Solar Activity
South America
Space Flight
Spacecraft
Audience
Scientific
Date
1996Metadata
Show full item recordDescription
Accessing the NASA trapped radiation models AP-8 and AE-8 with (B,L) values obtained with modern geomagnetic field models causes an unrealistic secular increase of the predicted flux over low altitude orbits. We show the secular variation of the orbit-averaged particle flux along the LDEF orbit and the mission dose, obtained using the AP-8 trapped radiation models with an epoch-dependent magnetic field. The artificially increased epoch-dependent fluxes and doses are compared to the flux and dose obtained with a consistent and more correct procedure for predicting fluxes with the NASA models. This procedure has been implemented in the radiation analysis software package UNIRAD developed and distributed by BIRA-IASB.
Citation
Heynderickx, D.; Lemaire, J.; Daly, E.J.; Evans, H.D.R. (1996). Calculating low-altitude trapped particle fluxes with the NASA models AP-8 and AE-8. , Radiation Measurements, Vol. 26, Issue 6, 947-952, DOI: 10.1016/S1350-4487(96)00096-0.Identifiers
scopus: 2-s2.0-0030273830
Type
Article
Peer-Review
Yes
Language
eng