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Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Displacement DamageMechanism and Effects
Christian PoiveyGordon Hopkinson
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Outline
• Introduction• Mechanism• NIEL concept
– Terms and units• Effect of Defects• Device Effects, examples• System Level Effects• Bibliography
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Introduction
• Semiconductor materials (Si, GaAs,..) are usually crystalline
• Space environment consists of energetic particles which can pass through shielding
• Leads to disruption in the lattice structure and device damage– Damage degrades electrical performances of
the device
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Displacement DamageVacancies and interstitials migrate, either recombine ( ~90%)or migrate and form stable defects (Frenkel pair)
I
V VStable Defect
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Displacement Damage• Energy of recoils (PKA spectrum) is
determined by the collision kinematics• electrons produce low energy PKAs• low energy protons (< 10 MeV in Si, higher in GaAs) : Coulomb (Rutherford) scattering dominates
• low energy PKAs
• neutrons and higher energy protons - nuclear elastic scattering and nuclear reactions (inelastic scattering)
• flat PKA spectrum
• above ~ 20 MeV in silicon, inelastic collisions tend to dominate
isolated (point) defects
cascades & multiple cascades
E
E
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Cascades
After Johnston, NSREC short course 2000
•50 keV PKA is typical of what can be produced by a 1MeV neutron or high energy proton•Threshold displacement energy in Si: 21 eV
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Non Ionizing Energy Loss (NIEL)
• Final concentration of defects depends only on NIEL (total energy that goes into displacements, about 0.1% of total energy loss) and not on the type an initial energy of the particle– Number of displacements (I-V pairs) is proportional to
PKA energy • Kinchin-Pease: N=T/2TD; T: PKA energy; TD: threshold energy to
create a Frenkel pair)
– In cascade regime the nature of the damage does not change with particle energy- just get more cascades
• nature of damage independent of PKA energy
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Non Ionizing Energy Loss (NIEL)• Assume underlying electrical effect
proportional to defect concentration (Shockley Read Hall theory)– Damage constant depends on device and parameter measured
damage = kdamage x displacement damage dose
dEdE
EdENIEL∫)()( φ
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Terms and Units• NIEL (displacement kerma = Kinetic Energy Released to
MAtter)– keVcm2/g or MeVcm2/g
• displacement damage dose DDD
DDD=∫NIEL(E)dΦ(E)dE (keV/g or MeV/g)dE
• Displacement damage equivalent fluence DDEF(monoenergetic beam)
FE0=∫(NIEL(E) dΦ(E)dENIEL(E0) dE
– e.g. 10 MeV protons/cm2 or 1 MeV neutrons/cm2
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
NIEL - Silicon
0.01
0.1
1
10
100
1000
0.1 1 10 100 1000Particle Energy (MeV)
NIEL
, (ke
Vcm
2/g)
Dale et al.Huhtinen and ArnioAkkerman et al.JunVasilescu & LindstroemASTM E 722Summers et al.Akkerman et al.
Electrons
Protons
Neutrons
Protons
Neutrons
Electrons
Si
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
NIEL - GaAs
0.001
0.01
0.1
1
10
100
1000
0.1 1 10 100 1000Energy (MeV)
NIE
L (k
eVcm
2 /g)
Summers et al.Akkerman et al.Summers et al.Akkerman et al.Akkerman et al.ASTM E 722
GaAs
Protons
Neutrons
Electrons
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Effect of Defects
Also: scattering at defects reduces carrier mobility, but only at vey high fluences
GenerationValence Band
CompensationTrappingRecombination Tunneling
EDONOR
Et
Conduction Band
EC
EV
Leakage Current
Minority CarrierLifetime
CTE in CCDsalso
Carrier Removal
Carrier Removal
Leakage Currentespecially if narrow bangap
and high electric field
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Device Effects – Lifetime Damage• Minority carrier lifetime
– affects bipolar ICs (e.g. wide base regions in lateral & substrate pnp transistors, >3 1010 50 MeV p/cm2)
– reduces detector responsivity (decrease in diffusion length, (Dτ)1/2)– reduces efficiency of solar cells– reduces light output of LEDs (non-radiative recombination)– threshold current increase in laser diodes– reduction of current transfer ratio (CTR) in optocouplers
• LED, phototransistor and coupling medium can be affected– sensitive devices can degrade at 1010 - 1011 50 MeV protons/cm2
Kφ
ττ+=
0
11
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Device Effects – Majority Carrier Removal• approximate carrier removal rates
• effect depends on doping (and whether n- or p- type)• for doping of 1015/cm3, carrier removal starts to be important for 50
MeV proton fluences ~ 1012 p/cm2
• but lightly doped structures can degrade at lower fluence (e.g. i-region of a p-i-n diode: due to leakage currents - 1010 p/cm2)
– but p-i-n diodes harder than conventional diodes since not sensitive to lifetime effects - collection by drift rather than diffusion
• type inversion (n- to p-type) in detectors & increase in depletion voltage
• carrier removal important for solar cells at high fluence
Particle Silicon GaAs
1 MeV 0.15/cm 0.6/cmelectrons
50 MeV 12/cm 30/cmprotons
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Device Effect - SummaryTechnology category sub-category Effects
General bipolar BJT hFE degradation in BJTs, particularly for low-current conditions (PNP devices more sensitive to DD than NPN)
diodes Increased leakage currentincreased forward voltage drop
Electro-optic sensors CCDs CTE degradation, Increased dark current, Increased hot spots, Increased bright columnsRandom telegraph signals
APS Increased dark current, Increased hot spots, Random telegraph signalsReduced responsivity
Photo diodes Reduced photocurrentsIncreased dark currents
Photo transistors hFE degradation??Reduced responsivity??Increased dark currents??
Light-emitting diodes LEDs (general) Reduced light power output
Laser diodes Reduced light power outputIncreased threshold current
Opto-couplers Reduced current transfer ratio
Solar cells SiliconGaAs, InP etc
Reduced short-circuit currentReduced open-circuit voltageReduced maximum power
Optical materials Alkali halidesSilica
Reduced transmission
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Device Effects - Examples
Rax et al. IEEE Trans.Nucl. Sci. vol 46(6), pp. 1660-1665, 1999
Voltage Regulator
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
0.00
0.20
0.40
0.60
0.80
1.00
1.20
0.E+00 2.E+10 4.E+10 6.E+10 8.E+10 1.E+11
Fluence (32 MeV protons/cm2)
CTR
0/CTR
#20 initial CTR=98
#29 initial CTR=81
#49 initial CTR=54
Mitel 3C91C (device is made no coupling medium)
5mA drive Vce=5V
Device Effects, Example
Reed et al. IEEE Trans. Nucl. Sci. vol 48(6), pp. 2202-2209, 2001
Optocoupler
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Device Effects - ExamplesLED
Johnston NSREC200 Short CourseNotes
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Device Effects - Examples
CCDDark Image:
dark spikes& CTI damage
1.8E10 10 MeV p/cm2
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Materials Effects• Effects in materials (insulators, optical glasses,
biological samples) are usually considered to be dominated by ionization processes– only a small fraction of the particle energy goes into
displacements– materials like insulators and glasses are disordered with no well
defined crystal structure (will contain many defects before irradiation)
– However displacement damage effects cannot be ruled out, particularly at the end of the particle track
• Displacement damage effects in photonic crystals tend to occur only at very high fluences
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Photonic Crystal
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
NIEL deviations: GaAs devices
But NIEL scaling is a good first approximationremoves most of the energy (and particle) dependencewithout it, testing/prediction would be much more complicated
Walters et al., IEEE Trans. Nucl. Sci., vol. 48, pp 1773-1777, 2001
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
System Level Effects• Sensor degradation important for payloads
and star trackers– but usually a gradual change in performance
• but difficult to calibrate (e.g. RTS and CTI effects in CCDs)• CTI effects for Chandra CCDs
• Optocouplers have failed in space applications– Topex Poseidon, failures in optocouplers in thruster
monitoring circuits at 2 x 1010 p/cm2
– optocouplers used in many types of circuit (e.g. DC-DC converters)
• Solar cell degradation or failure
Space Radiation and its Effects on EEE Components
EPFL Space Center 9th June 2009
Bibliography• RADECS short course notes
– 2003 Gordon HopkinsonRadiation Engineering Methods for Space Applications, part 3B: Radiation Effects and Analysis, Displacement Damage
• IEEE NSREC short course notes– 1999 Cheryl Marshall
Proton Effects and Test Issues for Satellite Designers, Part B: Displacement Effects
– 2000 Allan JohnstonOptoelectronic Devices with Complex Failure Modes