the radiation environment - nasa · pdf filethe radiation environment solar protons &...
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J. Barth/Code 562
The Radiation Environment
Solar Protons&
Heavier Ions
Galactic Cosmic Rays
Trapped Particles
Nikkei Science, Inc. of Japan, by K. Endo
J. Barth/Code 562
Components of the Natural Environment
u Transient» Galactic Cosmic Rays
− Protons & Heavier Ions» Solar Particle Events
− Protons & Heavier Ions
u Trapped» Electrons, Protons, & Heavier Ions
u Atmospheric & Terrestrial Secondaries» Neutrons
J. Barth/Code 562
Radiation & Effectsu Total Ionizing Dose
» Cumulative long termionizing damage due toprotons & electrons
u Displacement Damage» Cumulative long term non-
ionizing damage due toprotons, electrons, &neutrons
u Single Event Effects» Event caused by a single
charged particle - heavy ions& protons for some devices
E. Daly/ESA
J. Barth/Code 562
Sun
Yohkoh/SXT
SolarFlareu Dominates the
RadiationEnvironment» Source» Modulator
u Structure» Photosphere» Chromosphere» Corona
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Solar Windu Stream of Charged Particles from Sun’s
Corona» Electrons» Protons» Heavy Ions
u Magnetized Plasmau Detected Out to 10 billion km from Earth by
Pioneer 10u Velocity ~ 300 - 900 km/su Energy ~ .5 - 2.0 keV/nuc
Density ~ 1 - 30 / cm3}
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Solar Wind Density & Velocity
University of Maryland, SOHO/CELIAS
199723 Feb 25 Feb 27 Feb 29 Feb 1 Mar 3 Mar 5 Mar 7 Mar
300400
500
600
510152025
Den
sity
(#/c
m3 )
Velo
city
(km
/s)
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Magnetosphere
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Coronal Mass Ejections
Holloman AFB/SOON
u Bubble of Gas &Magnetic Field
u Ejects ~1017 gramsof Matter
u Shock WaveAcceleratesParticles toMillions of km/hr
u Associated withMagnetic Storms
u Proton Rich SolarEvents
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SOHO/LASCO During Solar Particle Event
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Solar Flares
u Sudden BrighteningNear Sunspots
u Solar System’sLargest ExplosiveEvents
u Particles AcceleratedDirectly by Event
u Heavy Ion Rich SolarEvents
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Magnetic Stormsu “Gusty” Solar Wind Disturbs the Current
Systems in the Magetosphereu Major Storms Probably the Result of CMEs
» Must Be Pointed Toward Earth» Strongest Arrive with Interplanetary Magnetic
Field Oriented Southu Cause Increase in Rate & Intensity of
Magnetic Sub-storms in the Geotail
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Electrical Currents
Discover Magazine - August 1995
u Normal Conditions» Currents Present on Quiet
Days
u Stormy Conditions» Intensified Currents
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Effects of Solar Stormsu Power Black-outs on Earthu Block Some Radio Communication
» Disturbs electrically charged gases in the ionosphereu Interfere with Cellular Phone Systems
» Ionospheric disturbances & satellite system failuresu Interfere with GPS Navigation (Ships & Airplanes)u Trigger Phantom Commands on Spacecraftu Increased Atmospheric Drag on Low Earth Orbit (LEO)
Satellitesu Increased Protons & Heavy Ion Particle Countsu “Pump Up” the Van Allen Belts
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1 6 11 16 21 25 311 6 11 16 21 25 31
Solar Wind Velocity (IMP-8 MIT) SAMPEX Electrons E > 1 MeV
Time of ANIK Failure
ANIK E1: Magnetic Storm
January 1994
Velo
city
(km
/s)
Coun
ts/s
(x10
)
8
1
23
4
5
6
7
0200
300
800
700
400
500
600
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Aurorau Particles stream down on
magnetic field lines from thegeomagnetic tail forming anauroral belt
u Electrons collide withatmospheric gases
u Electrons give energy to atomsand molecules which emitenergy as light
u Oxygen ---> Greenu Nitrogen ---> Red
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Aurora Borealis
u Northern lights ovalas measured byNOAA-14
u Centered on MagneticPole
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Early Warning: S-Curves
u Viewed with X-ray Imageryu Based on Two Years of
Observationsu Strong Correlation between
Sigmoid Regions and CMEsu Likely the Result of Twisted
Solar Magnetic Fieldsu May Provide Early Warning of
Particle Events
Montana State University
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Solar Activity: Cyclic Variationu Sunspot Cycle Discovered in mid 1800su Used as Indicator of Solar Activityu Increased Solar Activity Results in:
» Increased Rate of CMEs» Increased Rate of Solar Flares» Increased Rate of Magnetic Storms» Increased Levels of Electrons in Van Allen Belts» Decreased Levels of Protons in Van Allen Belts» Increased Incidence of New Belt Formation» Decreased Levels of Galactic Cosmic Rays» Increased Rate of Solar Particle Events
u Effects on Climate?
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Sunspot Cycle
1 7 5 0 1 8 0 0 1 8 5 0 1 9 0 0 1 9 5 0 2 0 0 00
5 0
1 0 0
1 5 0
2 0 0
2 5 0
Length Varies from 9 - 13 Years7 Years Solar Maximum, 4 Years Solar Minimum
Suns
pot N
umbe
rs
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1950 1960 1970 1980 1990 20000
50
100
150
200
250
Sunspot CycleSu
nspo
t Num
bers
Cycle 18
Cycle 22Cycle 21
Cycle 20
Cycle 19
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20
40
0
60
80
100
1930 19601940 1950 1970 1980 1990
150
0
100
200
50
Sunspot Cycle with Magnetic StormsA
nnua
l Num
ber o
f Day
s with
Ap>
4 Sunspots & Magnetic Storm Days
Ann
ual S
unsp
ot N
umbe
rSunspot Number# of Days with Ap > 4
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Solar Cycle - Aurora Days
From Way North Magazine
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Discovery of Galactic Cosmic Rays - 1913u Electroscope Experiments
» Dissipation of Charge on Leaves?» Emissions from Materials on Earth» “Clean” Instruments Did Not Eliminate Dissipation
u Hess» Balloon Experiments with Electroscopes» Hypothesis: Background Radiation Will Disappear with
Increasing Altitude» > 10,000 feet - Background Increased with Altitude» Named “Cosmic Rays” by Hess
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Galactic Cosmic Ray Ionsu All Elements in Periodic Table - 200 Million Years Oldu Energies in GeVu Found Everywhere in Interplanetary Spaceu Omnidirectionalu Mostly Fully Ionized - Protons & Bare Nuclei of Heavier
Elementsu Cyclic Variation in Fluence Levels
» Lowest Levels = Solar Maximum Peak» Highest Levels = Lowest Point in Solar Minimum
u Trajectories Bent by Magnetic Fieldu Single Event Effects Hazardu Model: CREME96
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1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0 9 0 1 0 01 0 -2
1 0 -1
1 0 0
1 0 1
1 0 2
1 0 3
1 0 4
1 0 5
1 0 6
1 0 7
1 0 8
1 0 9
1 0 1 0
GCRs: Nuclear CompositionRe
lativ
e Flu
x (S
i = 1
06 )
C
Nuclear Charge (Z)
HHe
OSi Fe
ZrBa Pt
PbIndividual Elements Even-Z Elements Elemental Groups
Energy = 2 GeV/n, Normalized to Silicon = 106
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GCRs: Solar Modulation
1 9 7 5 1 9 7 7 1 9 7 9 1 9 8 1 1 9 8 3 1 9 8 5 1 9 8 7 1 9 8 9 1 9 9 1 1 9 9 3 1 9 9 51 0 -5
1 0 -4
1 0 -3
1 0 -2
1 0 -1
1 0 0
1 0 1
1 0 2
Date
CNO
(#/c
m2 /
ster
/s/M
eV/n
)CNO - 24 Hour Averaged Mean Exposure Flux
Energy = 25-250 MeV/n - IMP-8
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1 0 -1 1 0 0 1 0 1 1 0 2 1 0 3 1 0 4 1 0 51 0 -6
1 0 -5
1 0 -4
1 0 -3
1 0 -2
1 0 -1
1 0 0
1 0 1
S u rfa c e I n c i d e n t1 0 0 m ils ( 2 . 5 4 m m ) A l5 0 0 m ils ( 1 2 . 7 m m ) A l
GCRs: Shielded Fluences - FePa
rticle
s (#/
cm2 /
day/
MeV
/n)
Interplanetary, CREME 96, Solar Minimum
Energy (MeV/n)
J. Barth/Code 562
1 0 -1 1 0 0 1 0 1 1 0 2 1 0 3 1 0 4 1 0 51 0 -6
1 0 -5
1 0 -4
1 0 -3
1 0 -2
1 0 -1
G E OG T OM E OE O SL E O
GCRsGCRs: Shielded: Shielded Fluences Fluences - Fe - FeCREME 96, Solar Minimum, 100 mils (2.54 mm) Al
Energy (MeV/nuc)Parti
cles (
#/cm
2 /da
y/M
eV/n
uc)
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Solar Particle Eventsu Increased Levels of Protons & Heavier Ionsu Energies
» Protons - 100s of MeV» Heavier Ions - 100s of GeV
u Abundances Dependent on Radial Distance from Sunu Partially Ionized - Greater Ability to Penetrate
Magnetosphereu Number & Intensity of Events Increases Dramatically
During Solar Maximumu Models
» Dose - SOLPRO, JPL, Xapsos/NRL» Single Event Effects - CREME96 (Protons & Heavier Ions)
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Solar Particle Events
u Poor Correlation with Solar Flaresu Strong Correlation with Coronal Mass Ejections
» No Fundamental Association with Flares» Transient Shock Wave Disturbances in the Solar Wind» Large Geomagnetic Storms» Large Particle Events
“The Solar Flare Myth” - Gosling
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Solar Particle Events
u Gradual ~ 10 per Year» Coronal Mass Ejection Driven Shocks» Same Elemental Abundances & Ionization States
as Coronal & Solar Wind Plasmau Impulsive ~ 1000 per Year
» Flare Accelerated» Abundances Characteristic of Interactions in the
Flare Plasma
“A New Paradigm” - Reames2 Types of Events
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Sunspot Cycle with Solar Proton Events
1 9 6 5 1 9 7 0 1 9 7 5 1 9 8 0 1 9 8 5 1 9 9 0 1 9 9 51 0 7
1 0 8
1 0 9
1 0 1 0
1 0 1 1> 1 0 M e V ; Φ ≥ 1 0 8 p /c m 2
> 3 0 M e V ; Φ ≥ 1 0 7 p /c m 2
Z u r i c h S m o o t h e d S u n s p o t N u m b e r
C y c l e 2 0 C y c l e 2 1 C y c le 22
*
**
0
2 0
4 0
6 0
8 0
1 0 0
1 2 0
1 4 0
1 6 0
1 8 0
2 0 0
Prot
ons (
#/cm
2 )
Year
Proton Event Fluences
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Modeling Approach
u Statistical Engineering Model» Intensity as a Function of Mission Duration & Confidence Level» Does Not Predict When Events Occur
u Use Maximum Entropy Principle - Incomplete Data Set» Determines Frequency Distribution of Large Solar Proton Events» Frequency Distribution Consistent with Other Complex Physical
Phenomena such as Earthquakesu Use Extreme Value Theory
» Determines Upper Limit for Occurrence of Huge Events» New Upper Limit Consistent with Data Sets Dating Back to
Ancient Times - Lunar Rock Record
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Solar Protons: Orbits
1 0 -1 1 0 0 1 0 1 1 0 2 1 0 3 1 0 4 1 0 5
e 2
1 0 -1 41 0 -1 31 0 -1 21 0 -1 11 0 -1 0
1 0 -91 0 -81 0 -71 0 -61 0 -51 0 -41 0 -31 0 -21 0 -11 0 01 0 11 0 21 0 31 0 4
GE
O
G E OE O SI = 6 0 d e g / H = 8 0 0 k mL E O
Energy (MeV)
Prot
ons (
#/cm
2 /se
c/M
eV)
Proton Levels Predicted by CREME 96
Averaged Over Worst Day
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TIROS Measurement of ProtonsDay Before Coronal Mass Ejection
H= 870/870 km
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TIROS Measurement of ProtonsNovember 6, 1997 Coronal Mass Ejection
H= 870/870 km
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Trapped Radiation
Trapped ParticlesProtons, Electrons, Heavy Ions
Nikkei Science, Inc. of Japan, by K. Endo
J. Barth/Code 562
Charged Particle Motionu Birkeland - 1895
» Vacuum chamber experiments to study aurora» With Poincare showed that charged particles spiraled around field
lines and are repelled by strong fieldsu Stöermer -
» Continued work of Birkeland on aurora» Calculations led to theory that there was a belt-like area around the
earth in which particles were reflected back and forth between thepoles
u Singer (U. o f Md) - 1957» Proposed that ring current could be carried by lower energy
particles injected by into trapped orbits by magnetic stormsu Christofilos
» Study of particle motion in magnetic fields - Project Argus
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Discovery of the Radiation Beltsu James Van Allen
» First Observation of AuroralElectrons with a Rocket
» Cosmic Ray Detectoru Highlight of US Participation
in IGY
Explorer I31 Jan 1958
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Trapped - Van Allen Beltsu Omnidirectionalu Components
» Protons: E ~ .04 - 500 MeV» Electrons: E ~ .04 - 7(?) MeV» Heavier Ions: Low E - Non-problem for Electronics
u Location of Peak Levels Depends on Energyu Average Counts Vary Slowly with the Solar Cycleu Location of Populations Shifts with Timeu Counts Can Increase by Orders of Magnitude During
Magnetic Storms» March 1991 Storm - Increases Were Long Term
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Proton Drift
Magnetic Field LineElectron Drift
Flux Tube
Trapped Particle Trajectory
Mirror Point
Conjugate Mirror Point
Trapped Particle MotionsSpiral, Bounce, Drift
after Hess
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Van Allen Belts
Inner Belt
Outer Belt
High Latitude Horns
Slot Region
BIRA/IASB
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Proton & Electron Intensities
1 2 3 4 5 6 7 8 9 101234
L-Shell
AP-8 Model AE-8 ModelEp > 10 MeV Ee > 1 MeV
NASA/GSFC
#/cm2/sec #/cm2/sec
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TIROS/NOAA Trapped Protons
1976 1980 1984 1988 1992 1996
104
103
102
101 50
100
150
200
250
Prot
on F
lux
(#/c
m2 /s
)
Date
Solar Cycle Variation: 80-215 MeV Protons
L=1.20
L=1.18
L=1.16
L=1.14
B/Bmin=1.0
Rad
io F
lux
F 10
.7
Huston et al.
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CRRES - Measured Proton Belt
AF Phillips Laboratory, SPD/GD
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Activity in the Slot Region - SAMPEX
Day (1992)
L-Sh
ell
190 250 310 370 430 490 550
5
3
11
9
7
1
SAMPEX/P1ADC: Electrons E > 0.4 MeV
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Magnetic Storms - HipparcosL-
Shel
l
4-Day, 9-Orbit Averages
Star Mapper - Radiation Background
Daly, et al.
March1990 1991 1992
2
4
6
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SRAM Upset Rates on CRUX/APEX
- 1 8 0 - 1 5 0 - 1 2 0 -90 -60 -30 0 3 0 60 9 0 1 2 0 1 5 0 1 8 0
L o n g i t u d e
-90
-75
-60
-45
-30
-15
0
1 5
3 0
4 5
6 0
7 5
9 0
Latit
ude
H i t a c h i 1 M :A l t i t u d e : 1 2 5 0 k m - 1 3 5 0 k m
1 . 0 E - 7 t o 5 . 0 E - 75 . 0 E - 7 t o 1 . 0 E - 61 . 0 E - 6 t o 5 . 0 E - 65 . 0 E - 6 t o 1 . 0 E - 51 . 0 E - 5 t o 5 . 0 E - 55 . 0 E - 5 t o 1 . 0 E - 41 . 0 E - 4 t o 5 . 0 E - 45 . 0 E - 4 t o 1 . 0 E - 31 . 0 E - 3 t o 5 . 0 E - 3
U p s e t s / B i t / D a y
-180 -150 -120 -90 -60 -30 0 30 60 90 120 150 180
Long i t ude
-90
-75
-60
-45
-30
-15
0
15
30
45
60
75
90
Latit
ude
Hi tach i 1M:A l t i t ude :650km - 750km
1 .0E-7 to 5 .0E-75 .0E-7 to 1 .0E-61 .0E-6 to 5 .0E-65 .0E-6 to 1 .0E-51 .0E-5 to 5 .0E-55 .0E-5 to 1 .0E-41 .0E-4 to 5 .0E-45 .0E-4 to 1 .0E-31 .0E-3 to 5 .0E-3
Upsets /B i t /Day
- 1 8 0 - 1 5 0 - 1 2 0 - 9 0 - 6 0 - 3 0 0 3 0 6 0 9 0 1 2 0 1 5 0 1 8 0
L o n g i t u d e
- 9 0
- 7 5
- 6 0
- 4 5
- 3 0
- 1 5
0
1 5
3 0
4 5
6 0
7 5
9 0
Latit
ude
H i t a c h i 1 M :A l t i t u d e : 1 7 5 0 k m - 1 8 5 0 k m
1 . 0 E - 7 t o 5 . 0 E - 75 . 0 E - 7 t o 1 . 0 E - 61 . 0 E - 6 t o 5 . 0 E - 65 . 0 E - 6 t o 1 . 0 E - 51 . 0 E - 5 t o 5 . 0 E - 55 . 0 E - 5 t o 1 . 0 E - 41 . 0 E - 4 t o 5 . 0 E - 45 . 0 E - 4 t o 1 . 0 E - 31 . 0 E - 3 t o 5 . 0 E - 3
U p s e t s / B i t / D a y
- 1 8 0 - 1 5 0 - 1 2 0 - 9 0 - 6 0 - 3 0 0 3 0 6 0 9 0 1 2 0 1 5 0 1 8 0
L o n g i t u d e
- 9 0
- 7 5
- 6 0
- 4 5
- 3 0
- 1 5
0
1 5
3 0
4 5
6 0
7 5
9 0
Latit
ude
H i t a c h i 1 M : A l t i t u d e : 2 4 5 0 k m - 2 5 5 0 k m
1 . 0 E - 7 t o 5 . 0 E - 75 . 0 E - 7 t o 1 . 0 E - 61 . 0 E - 6 t o 5 . 0 E - 65 . 0 E - 6 t o 1 . 0 E - 51 . 0 E - 5 t o 5 . 0 E - 55 . 0 E - 5 t o 1 . 0 E - 41 . 0 E - 4 t o 5 . 0 E - 45 . 0 E - 4 t o 1 . 0 E - 31 . 0 E - 3 t o 5 . 0 E - 3
U p s e t s / B i t / D a y
J. Barth/Code 562
Trapped Protons for E > 30 MeV(#/cm2/s) - Solar Minimum
-180 -150 -120 -90 -60 -30 0 30 60 90 120 150 180
-80
-60
-40
-20
0
20
40
60
80
1 10 100
1000
-180 -150 -120 -90 -60 -30 0 30 60 90 120 150 180
-80
-60
-40
-20
0
20
40
60
80
1
1
10
10
100
100
1000
1000
0
-180 -150 -120 -90 -60 -30 0 30 60 90 120 150 180
-80
-60
-40
-20
0
20
40
60
80
1
1
10
10
100
100
1000
1000
10000
10000
-180 -150 -120 -90 -60 -30 0 30 60 90 120 150 180
-80
-60
-40
-20
0
20
40
60
80
1
1
10
10
100
100
1000
1000
10000
J. Barth/Code 562
Particle Cascades in Atmosphere
u Collisions betweencosmic rays &atmospheric O & N
u Important product isneutrons
» Single Event Upsets− Shuttle− Aircraft− Ground
» Passenger & crewexposure in aircraft
J. Barth/Code 562
Neutronsu Source - Secondary Products of Particle
Cascades» Spacecraft Materials» Galactic Comic Ray Collisions with
Atmospheric O & Nu Single Event Upset Hazard
» Ground Level in Large Memory Banks» Avionics» Low Earth Orbits - Shuttle
u First Recognized as Problem in 1980s
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Neutron Environmentγ γ γ γ γ γγ γ γ γ γ γγ γ γ η η η η γ γ γ η η η ηγ γ γ γ γ γ η η η η η η η ηγ γ γ γ γ γγ γ γ γ γ γ η η η η η η η η γ γ γ γ η η η η η η η ηπ µ π υγ π γ η η η η γ µ γ η η η η
η η η η η η η ηγ π µ η η η η γ π µ η η η η η η η η η η η η
π µ η η η η π µ η η η ηπ µ γ π υ γ η η η η η η η η η ηπ µ π µ π µ γ γ η η
60,000 feet20,000 m
1,000,000 feet330 km
Ground ~ 1/500 of Peak Flux
150,000 feet50,000 m
γ Primary Cosmic Rays
η Neutrons
π,µ Secondary Cosmic Rays
Shuttle
Top ofAtmosphere
PeakNeutron
Flux
Aircraft
γ
η π,µN,O ~ 35,000 feet
10,000 m
Normand et al.
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20,000 40,000 60,000 80,000 100,000 120,000 140,0000.0
1.0
0.8
0.6
0.4
0.2
Neutron Flux Measurements
1-10 MeV & 10-100 MeV Energy Ranges
Altitude (feet)
Nor
mal
ized
to P
eak
Mendell/Holt1-10 MeV
Ait/Ouamer10-100 MeV Preszler/Saxzena
10-100 MeV
J. Barth/Code 562
1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0A lt i tu d e
0 .0
0 .2
0 .4
0 .6
0 .8
1 .0
1 .2
1 .4
Flux
Neutron Models: Flux vs. Altitude
Altitude ( Thousands of feet)
1-10 MeV Atmospheric Neutron Flux
1-10
MeV
Neu
tron
Flux
(n/c
m2 /
s)
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0 1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0 9 0La t i t ude
0.0
0 .2
0 .4
0 .6
0 .8
1 .0
1 .2
1 .4
Flux
Neutron Model: Flux vs. Latitude
Latitude (deg N)
1-10
MeV
Neu
tron
Flux
(n/c
m2 /
s)
1-10 MeV Atmospheric Neutron Flux
Averaged Over Longitude
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Terrestrial Radiation Sources
u Man-madeuNatural Emissions from Earth Materials
» Package Contaminationu Cosmic Rays - Particle Showers
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Terrestrial Cosmic Rays
u Particles That Hit the Earth from Outer Spaceu Need > 1 GeV to Penetrate to Sea Levelu Fewer Than 1% Are Primaryu Mostly 3rd to 7th Generation Cascade Particlesu Search for Cause of Interference on Laboratory
Instruments in Early 1900s» Led to Discovery of Cosmic Rays by Hess
u Induce SEUs: Neutrons + Protons + Pions
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Terrestrial Cosmic Rays
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1 2 3 4 5 60
102030405060708090
18,94011,500
803 250 126
137,445
Total Counts = 169,064
E.B. Hughes & P.L. Marsden, 1966
Perc
enta
ge C
ontri
butio
n
Protons Muons Muons Pions Showers Neutrons (Captured) (in Flight)
IGY Neutron Monitor ResponseCosmic Ray Contributions at Sea Level
J. Barth/Code 562
1 2 3 4 5 6 7 8 9 1010-13
10-12
10-11
10-10
10-9
10-8
Sea Level10 Km
AM9114 4K NMOS Error Rates
Protons Neutrons Muons Pions Pions >100 MeV >10 MeV (Stopping) >100 MeV (Stopping)
Pred
icted
Err
ors /
Dev
ice /
s
Predicted Error Rates at Two Altitudes
J.F. Dicello, et al.., 1989
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Radiation Issues -Three Prime Technical Drivers
u COTS & Emerging Technologies» More sensitive to radiation» Some devices have new effects
u COTS - greater uncertainty about radiation hardness» Limited control» Frequent process changes
u Devices exposed to more radiation on-orbit» Use of composite materials in spacecraft structures» Shrinkage in spacecraft size & weight
Result:We are using more radiation sensitive components with less
protection